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United States. National Aeronautics and Space Administration
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Transonic wind tunnels

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1.
Analysis of fluctuating static pressure measurements in a large high Reynolds number transonic cryogenic wind tunnel
Author
Igoe, William B.
Published
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:108722
Format
Books / Microforms
2.
NASA Lewis 8- by 6-foot supersonic wind tunnel user manual
Author
Soeder, Ronald H.
Published
[Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:105771
Format
Books / Microforms
3.
Test of a trail [sic] cryogenic balance in the ONERA T2 wind tunnel
Published
Washington, DC : National Aeronautics and Space Administration, [1987]
Location
SML, Microform (Non-Circulating) >> NAS 1.77:20078
Format
Books / Microforms
4.
Investigation of the components of the NAL high Reynolds number two-dimensional wind tunnel. Part IV, Design, construction, and performance of the exhaust silencer
Published
Washington D.C. : National Aeronautics and Space Administration, [1986]
Location
SML, Microform (Non-Circulating) >> NAS 1.15:88513
Format
Books / Microforms
5.
Design features and operational characteristics of the Langley 0.3-meter transonic cryogenic tunnel
Author
Kilgore, Robert A.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976.
Location
Library Shelving Facility (LSF) >> NASA TN D-8304
Format
Books
6.
Transonic and supersonic test of a Mach 2.65 mixed-compression axisymmetric intake
Author
Koncsek, J. L.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Virginia 22151], 1972.
Location
Library Shelving Facility (LSF) >> NASA CR-1977
Format
Books
7.
Numerical calculation of transonic flow about slender bodies of revolution
Author
Bailey, Frank R.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971.
Location
Library Shelving Facility (LSF) >> NASA TN D-6582
Format
Books
8.
Effect of plug base contour on performance of a fully truncated plug nozzle with translating shroud
Author
Mercer, Charles E.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970.
Location
Library Shelving Facility (LSF) >> NASA TN D-5655
Format
Books
9.
Evaluation of a technique for determining airplane aileron effectiveness and roll rate by using an aeroelastically scaled model
Author
Abel, Irving
Published
Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969.
Location
Library Shelving Facility (LSF) >> NASA TN D-5538
Format
Books
10.
A theoretical and experimental study of unsteady flow processes in a Ludwieg tube wind tunnel
Author
Warmbrod, John D.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969.
Location
Library Shelving Facility (LSF) >> NASA TN D-5469
Format
Books
11.
Determination of boundary-reflected-disturbance lengths in the Langley 16-foot transonic tunnel
Author
Capone, Francis J.
Published
Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967.
Location
Library Shelving Facility (LSF) >> NASA TN D-4153
Format
Books
12.
Rolling stability derivatives of a variable-sweep tactical fighter model at subsonic and transonic speeds
Author
Henderson, William P.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1967.
Location
Library Shelving Facility (LSF) >> NASA TN D-3845
Format
Books
13.
Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84
Author
Loving, Donald L.
Published
Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967.
Location
Library Shelving Facility (LSF) >> NASA TN D-4021
Format
Books
14.
Technique for verifying structural integrity of full-scale segments of launch vehicles at transonic speeds
Author
Blaha, Bernard J.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1967.
Location
Library Shelving Facility (LSF) >> NASA TN D-3876
Format
Books
15.
Transonic aerodynamic characteristics of a model of a supersonic fighter-bomber airplane with external fuel tanks and other modifications
Author
Ferris, James C.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966.
Location
Library Shelving Facility (LSF) >> NASA TN D-3701
Format
Books
16.
Transonic aerodynamic investigation of tension shell and blunted 100 ̊conical shapes for unmanned entry vehicles
Author
Harris, Charles D., 1952-
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966.
Location
Library Shelving Facility (LSF) >> NASA TN D-3700
Format
Books
17.
Effect of rearward body strakes on the transonic aerodynamic characteristics of an unswept-wing fighter aircraft
Author
Carter, C. Robert
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Virginia 22151], 1965.
Location
Library Shelving Facility (LSF) >> NASA TN D-3011
Format
Books
18.
Transonic aerodynamic characteristics of a Saturn IB-Apollo launch vehicle with various upper-stage configurations
Author
Carter, C. Robert
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Virginia 22151], 1965.
Location
Library Shelving Facility (LSF) >> NASA TN D-2829
Format
Books
19.
Measured and calculated subsonic and transonic flutter characteristics of a 45 ̊sweptback wing planform in air and in freon-12 in the Langley transonic dynamics tunnel
Author
Yates, E. Carson (Edward Carson), 1926-
Published
Washington, D.C. : National Aeronautics and Space Administration, 1963.
Location
Library Shelving Facility (LSF) >> NASA TN D-1616
Format
Books
20.
Steady-state characteristics of a differential-pressure system for evaluating angles of attack and sideslip of the Ranger IV vehicle
Author
Yates, E. Carson (Edward Carson), 1926-
Published
Washington, D.C. : National Aeronautics and Space Administration, 1963.
Location
Library Shelving Facility (LSF) >> NASA TN D-1966
Format
Books
21.
Surface pressure distributions on 0.0628-scale models of proposed project fire space vehicles at Mach numbers from 0.25 to 4.63
Author
Pearson, Albin O.
Published
Washington, D.C. : National Aeronautics and Space Administration, 1963.
Location
Library Shelving Facility (LSF) >> NASA TN D-1961
Format
Books
22.
A rigidly forced oscillation system for meaasuring dynamic-stability parameters in transonic and supersonic wind tunnels
Author
Braslow, Albert L.
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]
Location
Library Shelving Facility (LSF) >> NASZ TN D-1231
Format
Books
23.
Aerodynamic loading characteristics at Mach numbers from 0.80 to 1.20 of a 1/10-scale three-stage scout model
Author
Kelly, Thomas C.
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1961.
Location
Library Shelving Facility (LSF) >> NASA TN D-945
Format
Books
24.
Low subsonic pressure distributions on three rigid wings simulating paragliders with varied canopy curvature and leading-edge sweep
Author
Fournier, Paul G.
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1961.
Location
Library Shelving Facility (LSF) >> NASA TN D-983
Format
Books
25.
Transonic aerodynamic loading characteristics of a wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for a design Mach number [square root of] 2
Author
Cassetti, Marlowe D.
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1961.
Location
Library Shelving Facility (LSF) >> NASA TN D-971
Format
Books
26.
Transonic wind-tunnel tests of an error-compensated static-pressure probe
Author
Capone, Francis J.
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1961.
Location
Library Shelving Facility (LSF) >> NASA TN D-961
Format
Books
27.
Experimental investigation at transonic speeds of pressure distributions over wedge and circular-arc airfoil sections and evaluation of perforated-wall interference
Author
Knechtel, Earl D. (Earl Dennis)
Published
Washington, D.C. : National Aeronautics and Space Administration, 1959.
Location
Library Shelving Facility (LSF) >> NASA TN D-15
Format
Books