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Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability [microform] / David J. Wing, Charles T.L. Mills, and Mary L. Mason.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
1997
0 resources
Comparison of turbulence models for nozzle-afterbody flows with propulsive jets [microform] / William B. Compton III.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
1999
0 resources
Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf [microform] / Milton Lamb and John G. Taylor, Mark C. Frassinelli.
Microform
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1996]
1996
0 resources
Nozzle thrust optimization while reducing jet noise [microform] / J.M. Seiner, M.M. Gilinsky.
Microform
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight [microform] / K. Yamamoto ... [et al.].
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1984.
1984
0 resources
Vacuum chamber pressure effects on thrust measurements of low Reynolds number nozzles [microform] / James S. Sovey ... [et al.].
Microform
[Washington, D.C.] : National Aeronautics and Space Administration, [1985]
1985
1 resource