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Theoretical studies of a molecular beam generator [microform] : progress report for the period ended May 15, 1994 / by John Heinbockel, principal investigator.
Text
Norfolk, Va. : Dept. of Mathematics & Statistics, College of Sciences, Old Dominion University ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
A theory and experiments for detecting shock locations [microform] / S.I. Hariharan and D.K. Johnston and G. Adamovsky.
Text
Washington, DC : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.
Text
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
1991
0 resources
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles [microform] / Craig A. Hunter.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle [microform] / David J. Wing.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels [microform] / Milton Lamb.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows [microform] / by Scott T. Imlay.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, 1986.
1986
0 resources
High speed nozzles task [microform] : final report / Awatef Hamed, principal investigator.
Text
[Cincinnati, Ohio?] : University of Cincinnati ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Optical techniques for shock visualization and detection [microform] / G. Adamovsky and D.K. Johnson.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Nozzle flow with vibrational nonequilibrium [microform] : final report for the period ended August 31, 1995 / by J.H. Heinbockel, principal investigator and J.G. Landry, graduate research assistant.
Text
Norfolk, Va. : Old Dominion University Research Foundation, Dept. of Mathematics & Statistics, College of Sciences ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Direct numerical simulation of acoustic waves interacting with a shock wave in a quasi-1D convergent-divergent nozzle using an unstructured finite volume algorithm [microform] / Trong T. Bui and Reda R. Mankbadi.
Text
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Nozzle flow with vibrational nonequilibrium [microform] / by John Gary Landry.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Screech tones from rectangular jets with spanwise oblique shock-cell structures [microform] : [final contractor report] / Ganesh Raman.
Text
[Cleveland, Ohio] : National Aeronautics and Space Administration, [Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
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.
Text
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.
Text
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.
Text
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.
Text
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.
Text
[Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.
Text
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, [1991]
1991
0 resources
Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles [microform] / Mary L. Mason and Bobby L. Berrier.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
1985
0 resources
Experimental investigation of shock-cell noise reduction for single-stream nozzles in simulated flight [microform] / K. Yamamoto ... [et al.].
Text
[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.].
Text
[Washington, D.C.] : National Aeronautics and Space Administration, [1985]
1985
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS104805Exhaust nozzle plume and shock wave interaction / Raymond S. Castner, Alaa Elmiligui, Susan Cliff.
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013.
2013
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo51485Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / Daniel S. Jones [and four others].
Text
Edwards, CA : National Aeronautics and Space Administration, Armstrong Flight Research Center, October 2014.
2014-10
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo58350Transonic investigation of two-dimensional nozzles designed for supersonic cruise / Francis J. Capone and Karen A. Deere.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2015.
2015-8
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo62838Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / Daniel E. Paxson [and three others].
Text
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2015.
2015-8
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo62842Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf / Milton Lamb and John G. Taylor, Mark C. Frassinelli.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, September 1996.
1996-9
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo65363Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft / Bobby L. Berrier and Richard J. Re.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
1980-12
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo71372Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / Jeffery A. Yetter, Laurance D. Leavitt.
Text
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
1980-12
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo71384No results found from Digital Research Books Beta
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