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United States. National Aeronautics and Space Administration. Scientific and Technical Information Program
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Aerodynamics Supersonic

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Current results range from 1991 to 1993

1.
Analytical and experimental studies of a short compact subsonic diffuser for a two-dimensional supersonic inlet
Author
Iek, Chanthy
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3247
Format
Books / Microforms
2.
Automatic computation of wing-fuselage intersection lines and fillet inserts with fixed-area constraint
Author
Barger, Raymond L.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4406
Format
Books / Microforms
3.
Experimental effects of wing location on wing-body pressures at supersonic speeds
Author
Allen, Jerry M.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4434
Format
Books / Microforms
4.
An experimental investigation of a Mach 3.0 high-speed civil transport at supersonic speeds
Author
Hernandez, Gloria
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3365
Format
Books / Microforms
5.
Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration
Author
Cox, Mike C.
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], 1993.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3355
Format
Books / Microforms
6.
Effect of planform and body on supersonic aerodynamics of multibody configurations
Author
McMillin, S. Naomi (Susan Naomi)
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 1.60:3212
Format
Books / Microforms
7.
Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55⁰ cropped delta wing
Author
Erickson, Gary 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 1.60:3253
Format
Books / Microforms
8.
Flight test results of riblets at supersonic speeds
Author
Zuniga, Fanny A.
Published
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.15:4387
Format
Books / Microforms
9.
Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds
Author
Wood, Richard M.
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 1.60:3105
Format
Books / Microforms
10.
Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5
Author
Covell, Peter F.
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 1.15:4337
Format
Books / Microforms
11.
The natural flow wing-design concept
Author
Wood, Richard M.
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 1.60:3193
Format
Books / Microforms
12.
Secondary instability of high-speed flows and the influence of wall cooling and suction
Author
El-Hady, Nabil M.
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
Location
SML, Microform (Non-Circulating) >> NAS 1.26:4427
Format
Books / Microforms
13.
Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design
Author
Carlson, Harry W.
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 1.60:3202
Format
Books / Microforms
14.
Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows
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
http://purl.access.gpo.gov/GPO/LPS67809
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3142
Format
Books / Microforms
15.
Transonic and supersonic Euler computations of vortex-dominated flow fields about a generic fighter
Author
Goodsell, Aga M.
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], 1991.
Location
SML, Microform (Non-Circulating) >> NAS 1.60:3156
Format
Books / Microforms