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1
A low speed wind tunnel study of vortex interaction control techniques on a chine-forebody/delta-wing configuration
by Rao, Dhanvada M.
Hampton, Va. : [Springfield, Va.? : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service [distributor], 1992

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Government Document Book
2
Effect of wing design on the longitudinal aerodynamic characteristics of a wing-body model at subsonic speeds /
by Henderson, William P., Huffman, Jarrett K.
Washington, D.C. : National Aeronautics and Space Administration, 1972

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Government Document Book
3
Low subsonic flight and force investigation of a supersonic transport model with a variable-sweep wing /
by Freeman, Delma C.
Washington, D.C. : National Aeronautics and Space Administration, 1968

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document Book
4
Laminar flow control perforated wing panel development /
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1986

Government Document Book
5
The multiple-function multi-input/multi-output digital controller system for the AFW wind-tunnel model /
by Hoadley, Sherwood T. (Sherwood Tiffany)
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [For sale by the National Technical Information Service], 1992

Government Document Book
6
Low-speed static wind-tunnel investigation of a half-span fuselage and variable-sweep pressure wing model /
by Lamar, John E.
Washington, D.C. : National Aeronautics and Space Administration, 1971

Government Document Book
7
Calculated wind-tunnel-boundary lift-interference factors for rectangular perforated test sections /
by Schilling, Benferd L.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information], 1970

Government Document Book
8
Residual strength and crack propagation tests on C-130 airplane center wings with service-imposed fatigue damage /
by Snider, H. Lawrence
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor], 1972

Government Document Book
9
Novel composites for wing and fuselage applications : textile reinforced composites and design guidelines /
Hampton, Va. : Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1996

Government Document Book
10
Novel composites for wing and fuselage applications.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996

Government Document Book
11
Comparison of several methods for estimating low-speed stability derivatives for two airplane configurations /
by Fletcher, Herman S.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971

Government Document Book
12
Application of phase-change technique to thin sections with heating on both surfaces /
by Hunt, James L. (James Larry), 1939-
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1973

Government Document Book
13
Investigation of the static lift capability of a low-aspect-ratio wing operating in a powered ground-effect mode /
by Huffman, Jarrett K.
Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1974

Government Document Book
14
Prediction of effects of wing contour modifications on low-speed maximum lift and transonic performance for the EA-6B aircraft /
by Allison, Dennis O.
Washington, D.C. : Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service, 1990

Government Document Book
15
Aerodynamic and deployment characteristics of multistage canopy and suspension-line reefing systems for a twin-keel all-flexible parawing /
by Morgan, Harry L.
Washington, D.C. : Springfield, VA : National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971

Government Document Book
16
Results of design studies and wind tunnel tests of high-aspect-ratio supercritical wings for an energy efficient transport /
by Steckel, Doris K.
Hampton, Va. : The Center, 1980

Government Document Book
17
Instability and transition of flow at, and near, an attachment-line : including control by surface suction /
by Smith, A.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1998

Government Document Book
18
Low subsonic flight and force investigation of a supersonic transport model with a double-delta wing /
by Freeman, Delma C.
Washington, D.C. : National Aeronautics and Space Administration, 1968

Government Document Book
19
Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /
by Mack, Robert J.
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999

Government Document Book
20
Stereo-video data reduction of wake vortices and trailing aircrafts /
by Alter-Gartenberg, Rachel
Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1998

Government Document Book
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