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1.
Applications of circulation control technologies
Published
Reston, VA : American Institute of Aeronautics and Astronautics, ©2006.
Online
Online book
Location
Yale Internet Resource >> None
Format
Books / Online
2.
Ice accretions and icing effects for modern airfoils
Author
Addy, Harold E., Jr., 1960-
Published
Cleveland, Ohio : National Aeronautics Administration, Glenn Research Center, [2000]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
3.
Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques
Author
Mineck, Raymond E.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
4.
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : evaluation of initial perforated configuration
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
5.
The effects of winglets on low aspect ratio wings at supersonic Mach numbers
Author
Keenan, James A. (James Anthony), 1966-
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
6.
Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil
Author
Hahne, David E. (David Edgar)
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
7.
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis
Author
Brooks, Cuyler W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
8.
A study of residual interference effects in adaptive wall testing of a 7-inch chord CAST-10-2/DOA 2 airfoil model
Author
Murthy, A. V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
9.
A unified viscous theory of lift and drag of 2-D thin airfoils and 3-D thin wings
Author
Yates, John E.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
10.
Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels
Author
Green, Lawrence L. (Lawrence Lee)
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
11.
Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade
Author
Noonan, Kevin W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
12.
A direct-inverse method for transonic and separated flows about airfoils
Author
Carlson, Leland A.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
13.
Heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis Icing Research Tunnel
Author
Poinsatte, Philip E.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
14.
NASA supercritical airfoils : a matrix of family-related airfoils
Author
Harris, Charles D., 1952-
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
15.
CAST-10-2/DOA 2 Airfoil Studies Workshop results : proceedings of a workshop
Author
CAST-10-2/DOA 2 Airfoil Studies Workshop
Published
Washington, D.C. : NASA, Office of Management, Scientific and Technical Information Division, 1989.
Online
Online book
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
16.
The NASA Langley laminar-flow-control experiment on a swept supercritical airfoil : basic results for slotted configuration
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
17.
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : drag euqations
Author
Brooks, Cuyler W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
18.
NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
Author
Jenkins, Renaldo V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
19.
Numerical simulation and comparison of symmetrical/supercritical airfoils for the near tip region of a helicopter in forward flight
Author
Badavi, F. F.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
20.
Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel
Author
Jenkins, Renaldo V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
21.
Aerofoil testing in a self-streamlining flexible walled wind tunnel
Author
Lewis, Mark Charles
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
22.
Effect of advanced rotorcraft airfoil sections on the hover performance of a small-scale rotor model
Author
Althoff, Susan L.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
23.
Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section
Author
Ladson, Charles L.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
24.
Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley low-turbulence pressure tunnel
Author
McGhee, Robert J.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
25.
Simulation of two-dimensional viscous flow through cascades using a semi-elliptic analysis and hybrid C-H grids
Author
Ramamurti, R.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
26.
Technology for pressure-instrumented thin airfoil models
Author
Wigley, David A.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
27.
An analysis of the crossover between local and massive separation on airfoils
Author
Burnett, M.
Published
Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
28.
Lewis inverse design code (LINDES) : users manual
Author
Sanz, Jose M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
29.
Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil
Author
Ferris, James C.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
30.
Proceedings of the Circulation-Control Workshop 1986
Author
Circulation-Control Workshop
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
Online
no.2432 1987
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
31.
A simplified fourwall interference assessment procedure for airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel
Author
Murthy, A. V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
32.
TRANDESNF : a computer program for transonic airfoil design and analysis in nonuniform flow
Author
Chang, Jen-Fu
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
33.
Wall interference tests of a CAST 10-2/DOA 2 airfoil in an adaptive-wall test section
Author
Mineck, Raymond E.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
34.
Wind-tunnel investigation of a full-scale general aviation airplane equipped with an advanced natural laminar flow wing
Author
Murri, Daniel G.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
35.
The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers
Author
Plentovich, Elizabeth B.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
36.
R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
Author
Jenkins, Renaldo V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
37.
Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads
Author
Batina, John T.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
38.
High Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author
Johnson, William G. (William Garland), 1944-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
39.
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author
Johnson, William G. (William Garland), 1944-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
40.
Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Author
Johnson, William G. (William Garland), 1944-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
41.
Static and dynamic pressure measurements on a NACA 0012 airfoil in the Ames High Reynolds Number Facility
Author
McDevitt, John B.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
42.
Airfoil interaction with an impinging vortex
Author
McAlister, Kenneth W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [St. Louis, Mo.] : U.S. Army Aviation Systems Command ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Online
Online book
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
43.
Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
Author
Jenkins, Renaldo V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
44.
Design and experimental results for a flapped natural-laminar-flow airfoil for general aviation applications
Author
Somers, Dan M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
45.
Design and experimental results for a Natural-Laminar-Flow airfoil for general aviation application
Author
Somers, Dan M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
46.
Evaluation of turbulence reduction devices for the Langley 8-foot Transonic Pressure Tunnel
Author
McKinney, Marion O.
Published
Washington, D.C. : National Aeronautics and Space Administration, 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
47.
Historical background and design evolution of the transonic aircraft technology supercritical wing
Author
Ayers, Theodore G.
Published
Washington, D.C. : National Aeronautical and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
48.
Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions
Author
Florschuetz, L. W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
49.
Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63₁-012 airfoil
Author
Yu, James C.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
50.
A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation
Author
Barnwell, Richard W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
51.
Wind-tunnel results for a modified 17-percent-thick low-speed airfoil section
Author
McGhee, Robert J.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
52.
Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
Author
Noonan, Kevin W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
53.
Comparison of elastic and elastic-plastic structural analyses for cooled turbine blade airfoils
Author
Kaufman, Albert, 1928-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
54.
A computer program for the design and analysis of low-speed airfoils
Author
Eppler, Richard A.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
55.
Evaluation of flow quality in two large NASA wind tunnels at transonic speeds
Author
Harvey, Bill
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
56.
Investigation of blown boundary layers with an improved wall jet system
Author
Saripalli, K. R.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
57.
A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations
Author
Davis, Joseph E. (Joseph Eugene), 1946-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
58.
Advanced technology airfoil research
Published
Washington, D.C. : National Aeronautics and Space Administration, 1979-
Online
no.2045pt.1 1978
no.2045pt.2 1978
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
59.
Advanced technology airfoil research : proceedings of a conference held at Langley Research Center, Hampton, Virginia, March 7-9, 1978
Author
NASA Conference on Advanced Technology Airfoil Research
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office : U.S. Govt. Print. Off., 1979-
Online
pt.1-2
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
60.
Approximation concepts for numerical airfoil optimization
Author
Vanderplaats, Garret N.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
61.
Effects of upper surface modification on the aerodynamic characteristics of the NACA 632-215 airfoil section
Author
Hicks, R. M. (Raymond Morton), 1932-
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
62.
Experimental investigation of three helicopter rotor airfoils designed analytically
Author
Bingham, Gene J.
Published
Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
63.
Leading-edge slat optimization for maximum airfoil lift
Author
Olson, Lawrence E.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
64.
Airfoil design by numerical optimization using a minicomputer
Author
Hicks, R. M. (Raymond Morton), 1932-
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
65.
Analysis of a theoretically optimized transonic airfoil
Author
Lores, M. E.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
66.
Application of shock tubes to transonic airfoil testing at high Reynolds numbers
Author
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
67.
Correlation of laser velocimeter measurements over a wing with results of two prediction techniques
Published
Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
68.
Dynamic stall experiments on the NACA 0012 airfoil
Author
McAlister, Kenneth W.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
69.
Erosion/corrosion of turbine airfoil materials in the high-velocity effluent of a pressurized fulidized coal combustor
Author
Zellers, Glenn R.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
70.
Flight evaluation of the transonic stability and control charcteristics of an airplane incorporating a supercritical wing
Author
Matheny, Neil W.
Published
Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
71.
Low-speed aerodynamic characteristics of a 16-percent thick variable-geometry airfoil designed for general aviation applications
Author
Barnwell, Richard W.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
72.
Operational manual for two-dimensional transonic code TSFOIL
Author
Stahara, Stephen S.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
73.
Water-tunnel experiments on an oscillating airfoil at RE = 21,000
Author
McAlister, Kenneth W.
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
74.
Boundary-fitted curvilinear coordinate systems for solution of partial differential equations on fields containing any number of arbitrary two-dimensional bodies
Author
Thompson, Joe F.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
75.
Experimental and theoretical low-speed aerodynamic characterisitics of a Wortmann airfoil as manufactured on a fiberglass sailplane
Author
Somers, Dan M.
Published
Washington : National Aeronautics and Space Administration : Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
76.
An experimental evaluation of the application of the Kirchhoff formulation for sound radiation fron an oscillating airfoil
Author
Brooks, Thomas F.
Published
[Washington] : National Aeronoautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
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Books / Online
77.
Finite state modeling of aeroelastic systems
Author
Vepa, Ranjan
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
78.
A low speed two-dimensional study of flow separation on the GA(W)-1 airfoil with 30-percent chord Fowler flap
Author
Seetharam, H. C.
Published
Washington, D.C. : National Aeronautics and Space Administration, [1977]
Online
Online book
Location
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79.
Measurements of surface-pressure and wake-flow fluctations in the flow field of a Whitcomb supercritical airfoil
Author
Roos, Frederick W.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
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80.
Prediction of light aircraft horizontal tail onset flows : a review and analysis
Author
Summey, Delbert Clyde, 1946-
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
81.
Trandes : a Fortran program for transonic airfoil analysis or design
Author
Carlson, Leland A.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
82.
Transonic wind-tunnel investigation of the maneuver potential of the NASA supercritical wing concept : phase I
Author
Hallissy, James B.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
83.
Two-dimensional wind tunnel test of an oscillating rotor airfoil, volume I
Author
Dadone, L. U. (Leo U.)
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
84.
Two-dimensional wind tunnel test of an oscillating rotor airfoil, volume II
Author
Dadone, L. U. (Leo U.)
Published
[Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
85.
Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence
Author
Paterson, Robert W. (Robert William), 1939-
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
86.
The effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil section, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems
Author
Dods, Jules B.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976.
Online
Online book
Location
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Books / Online
87.
An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0
Author
Re, Richard J.
Published
Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
88.
Transonic airfoil design using cartesian coordinates
Author
Carlson, Leland A.
Published
Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976.
Online
Online book
Location
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Books / Online
89.
US Army helicopter design datcom
Author
Dadone, L. U.
Published
St. Louis, MO. : Army Aviation Systems Command, 1976-
Online
v.1
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
90.
Adaptation of the Theodorsen theory to the representation of an airfoil as a combination of a lifting line and a thickness distribution
Author
Barger, Raymond L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
91.
Application of numerical optimization to the design of low-speed airfoils
Author
Hicks, R. M. (Raymond Morton), 1932-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
92.
Detailed transonic flow field measurements about a supercritical airfoil section
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
93.
Development of a computer program to obtain ordinates for NACA 4-digit, 4-digit modified, 5-digit, and 16-series airfoils
Author
Ladson, Charles L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
94.
Effects of forward contour modification on the aerodynamic characteristics of the NACA 64₁-212 airfoil section
Author
Hicks, R. M. (Raymond Morton), 1932-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
95.
Experimental and theoretical low-speed aerodynamic characteristics of the NACA 65₁-213, a = 0.50 airfoil
Author
Beasley, William D.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
96.
Experimental studies of flow separation and stalling on a two-dimensional airfoil at low speeds
Author
Seetharam, H. C.
Published
Washington, D.C. : National Aeronautics and Space Administration, 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
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Books / Online
97.
High Reynolds number test of a NACA 65₁-213, a = 0.5 airfoil at transonic speeds
Author
Burdges, Kenneth P.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
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Books / Online
98.
Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections
Author
Goradia, Suresh H. (Suresh Harkisondas), 1937-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
99.
Transonic airfoil flowfield analysis using Cartesian coordinates
Author
Carlson, Leland A.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
100.
An assessment of airfoil design by numerical optimization
Author
Hicks, R. M. (Raymond Morton), 1932-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online