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Aeroservoelastic testing of free flying wind tunnel models

Scott, Robert C., author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013. 2013

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

Design study of advanced model support systems for the National Transonic Facility

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1987] 1987

Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall

Everhart, Joel L.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994] 1994

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Met

Lawing, Pierce L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980. 1980-

Modeling and control study of the NASA 0.3-meter transonic cryogenic tunnel for use with sulfur hexa

Balakrishna, S., 1931-
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992] 1992

Modifications to Langley 0.3-m TCT adaptive wall software for heavy gas test medium.

Murthy, A. V.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992] 1992

The NASA Langley 16-foot transonic tunnel historical overview, facility description, calibration, fl

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995] 1995

New coherent optical techniques for National Transonic Wind Tunnel Facility

Casasent, D. P. (David Paul), author.
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 1984. 1984-

Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to

Berrier, Bobby L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1984. 1984-