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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-

Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability

Bangert, Linda S.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989. 1989

Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design w

Leavitt, Laurence D.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985. 1985

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-