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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-

Flow unsteadiness effects on boundary layers

Murthy, Sreedhara V.
[Moffett Field, Calif. : NASA Ames Research Center, 1989] 1989

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