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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

Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor

Wilkes, Kevin, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, October 1996. 1996-

Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent ex

Yetter, Jeffery A., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight

Yamamoto, K., author.
Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, February, 1984. 1984-

A study of the sonic-boom characteristics of a blunt body at a Mach number of 6

Ashby, George C., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-