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1
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

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Government Document Book
2
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
3
Numerical study of three-dimensional separation and flow control at a wing-body junction progress report for the period ended April 30, 1989 /
by Lakshmanan, Balakrishnan, 1957-
Norfolk, Va. : Hampton, Va. : Department of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University ; National Aeronautics and Space Administration, Langley Research Center, 1989

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Government Document Thesis Electronic Book
4
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
5
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

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Government Document Book
6
Application of laminar flow control to supersonic transport configurations.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1990

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Government Document Book
7
Laminar flow control perforated wing panel development /
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 1986

Government Document Book
8
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
9
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
10
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
11
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
12
Measuring global surface pressures on a circulation control concept using pressure sensitive paint
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, 2012

This item is not available through EZBorrow. Please contact your institution’s interlibrary loan office for further assistance.
Government Document Electronic Book
13
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
14
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
15
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
16
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
17
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
18
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
19
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
20
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
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