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Interference (Aerodynamics)

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Online Results (60)
1.
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
2.
Comparison of a two-dimensional adaptive-wall technique with analytical wall interference correction techniques
Author
Mineck, Raymond E.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3132
Format
Books / Microforms
3.
Model representation in the PANCOR wall interference assessment code
Author
Al-Saadi, Jassim A.
Published
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:104152
Format
Books / Microforms
4.
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
5.
Wall-interference assessment and corrections for transonic NACA 0012 airfoil data from various wind tunnels
Author
Green, Lawerence L.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3070
Format
Books / Microforms
6.
Experimental study of pressure and heating rate on a swept cylindrical leading edge resulting from swept shock wave interference
Author
Glass, Christopher E. (Christopher Earl), 1955-
Published
[Washington, D.C.? : National Aeronautics and Space Administration, 1989]
Location
SML, Microform (Non-Circulating) >> NAS 1.26:185326
Format
Books / Microforms
7.
Computer simulation of a wind tunnel test section with discrete finite-length wall slots
Author
Kemp, William 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.
Location
Library Shelving Facility (LSF) >> NASA CR-3948
Format
Books
8.
Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing
Author
Lee, Edwin E.
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
9.
Propeller propulsion system integration : state of technology survey
Author
Miley, Stan 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, 1985.
Location
Library Shelving Facility (LSF) >> NASA CR-3882
Format
Books
10.
Study on needs for a magnetic suspension system operating with a transonic wind tunnel
Author
Martindale, William 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, 1985.
Location
Library Shelving Facility (LSF) >> NASA CR-3900
Format
Books
11.
Interference drag in a simulated wing-fuselage juncture
Author
Kubendran, L.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
12.
Interference drag in a simulated wing-fuselage juncture
Author
Kubendran, L.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Location
Library Shelving Facility (LSF) >> NASA CR-3811
Format
Books
13.
Support interference of wind tunnel models : a selective annotated bibliography
Author
Tuttle, Marie H.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
14.
Support interference of wind tunnel models : a selective annotated bibliography
Author
Tuttle, Marie H.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:81909/supp.
Format
Books / Microforms
15.
Support interference of wind tunnel models : a selective annotated bibliography
Author
Tuttle, Marie H.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984.
Location
Library Shelving Facility (LSF) >> NASA TM-81909
Format
Books
16.
Effects of axisymmetric and normal air jet plumes and solid plume on cylindrical afterbody pressure distributions at Mach numbers from 1.65 to 2.50
Author
Covell, Peter F.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
17.
Effects of axisymmetric and normal air jet plumes and solid plume on cylindrical afterbody pressure distributions at Mach numbers from 1.65 to 2.50
Author
Covell, Peter F.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:2005
Format
Books / Microforms
18.
Thermal design for areas of interference heating on actively cooled hypersonic aircraft
Author
Herring, R. L.
Published
Washington : National Aeronautics and Space Administration, Scientific and Technical Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
19.
Thermal design for areas of interference heating on actively cooled hypersonic aircraft
Author
Herring, R. L.
Published
Washington : National Aeronautics and Space Administration, Scientific and Technical Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978.
Location
Library Shelving Facility (LSF) >> NASA CR-2828
Format
Books
20.
Effect of nonlifting empennage surfaces on single-engine afterbody/nozzle drag at Mach numbers from 0.5 to 2.2
Author
Berrier, Bobby L.
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
21.
Effect of nonlifting empennage surfaces on single-engine afterbody/nozzle drag at Mach numbers from 0.5 to 2.2
Author
Berrier, Bobby L.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Location
Library Shelving Facility (LSF) >> NASA TN D-8326
Format
Books
22.
Wind tunnel and analytical investigation of over-the-wing propulsion/air frame interferences for a short-haul aircraft at Mach numbers from 0.6 to 0.78
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
23.
Wind tunnel and analytical investigation of over-the-wing propulsion/air frame interferences for a short-haul aircraft at Mach numbers from 0.6 to 0.78
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Location
Library Shelving Facility (LSF) >> NASA CR-2905
Format
Books
24.
Electromagnetic compatibility rationale report : conducted test requirements for electronic equipments in air transportation facilities
Author
Toler, J. C. (James Curtis), 1936-
Published
Washington, D.C. : Dept. of Transportation, Federal Aviation Administration, Systems Research and Development Service ; Springfield, Va. : For sale by the National Technical Information Service, [1976]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
25.
Effect of symmetrical vortex shedding on the longitudinal aerodynamic characteristics of wing-body-tail combinations
Author
Mendenhall, M. R.
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