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An airfoil flutter model suspension system to accommodate large static transonic airloads

Reed, Wilmer H.
Newport News, VA : DEI-Tech, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

Application of laminar flow control to supersonic transport configurations

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Contraction design for small low-speed wind tunnels

Bell, J. H.
[Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center ; Stanford, CA : Stanford University, Joint Institute for Aeronautics and Acoustics, [1988] 1988

Design and use of a guided weight impactor to impart barely visible impact damage

Lovejoy, Andrew E., author.
Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, April 2016. 2016-

Design concepts for cooled ceramic composite turbine vane

Boyle, Robert J., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2015. 2015-

Effects of velocity profile and inclination on dual-jet-induced pressures on a flat plate in a cross

Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speed

Plentovich, Elizabeth B.
[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. 1991

Enhanced design of turbo-jet LPT by separation control using phased plasma actuators

Corke, Thomas C.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Administration ; Springfield, VA : National Technical Information Service [distributor, 2003] 2003

An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic

Bartlett, Glynn R.
Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

Experimental investigation of unsteady flows at large incidence angles in a linear oscillating casca

Buffum, Daniel H., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996. 1996-

The fast scattering code (FSC) validation studies and program guidelines

Tinetti, Ana Fiorella, 1962-
Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Interaction of two-dimensional transverse jet with a supersonic mainstream

Kraemer, G. O.
Norfolk, Virginia : Department of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University ; Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 1983. 1983

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic

Hall, Robert M., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, April 1979. 1979-

Prediction of sound fields in acoustical cavities using the boundary element method

Kipp, Carl R.
West Lafayette, Ind. : Ray W. Herrick Laboratories, School of Mechanical Engineering, Purdue University ; [Washington, DC : National Aeronautics and Space Administration, 1985] 1985

Solar rocket plume/mirror interactions

Yu, Sheng-Tao.
[Washington, D.C.] : National Aeronautics and Space Administration, [1991] 1991

Unsteady potential flow past a propeller blade section

Takallu, Mohammad Ali, 1948-
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], 1990. 1990