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  • First NASA/Industry High Speed Research Program Nozzle Symposium [microform] / proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, November 17-19, 1992.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Final report for the NASA reload program [microform] / submitted by Atlantic Research Corporation.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
    • 1993

  • Enhancement of mixing in a rectangular jet by mechanical tabs [microform] / W.H. Brown and K.K. Ahuja.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1990]
    • 1990

  • Technical evaluation motor no. 5 (TEM-5) [microform] : final test report.

    • Text
    • Brigham City, UT : Thiokol Corporation, Space Operations ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Shear flow control of cold and heated rectangular jets by mechanical tabs [microform] / W.H. Brown and K.K. Ahuja.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • 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

  • Design and evaluation of thrust vectored nozzles using a multicomponent thrust stand [microform] : final progress report, 10-01-88 - 01-31-90 / Thomas W. Carpenter, principal investigator ... [et al.].

    • Text
    • San Luis Obispo, Calif. : California Polytechnic State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • Comparison of 3D computation and experiment for non-axisymmetric nozzles [microform] / H. Lai and E. Nelson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle [microform].

    • Text
    • [West Palm Beach, Fla. : Pratt and Whitney Aircraft ; Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989

  • 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

  • Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research [microform] : final report / Steven P. Schneider.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Automotive Stirling engine development program [microform] : semiannual technical progress report for period July 1-December 31, 1984 / Mechanical Technology Incorporated ; prepared for National Aeronautics and Space Administration, Lewis Research Center under contract DEN 3-32 ; for U.S. Department of Energy, Conservation and Renewable Energy, Office of Vehicle and Engine R&D.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
    • 1985

  • Numerical investigations in three-dimensional internal flows [microform] : semi-annual status report, 1 April through 30 September 1988 / by William C. Rose.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Star 48 solid rocket motor nozzle analyses and instrumented firings [microform] / Robert L. Porter.

    • 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

  • 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

  • Dual-throat thruster thermal model [microform] : final report / by R.L. Ewen, C.J. O'Brien, and L.W. Matthews.

    • Text
    • Sacramento, Calif. : Aerojet TechSystems Co. ; [Huntsville, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center, Alabama ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows [microform] : final grant report, NASA Langley grant NAG-1-1240, covering the period March 1991 to March 1993 / Darshan Dosanjh, Eric F. Spina.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Laser doppler velocimeter system for subsonic jet mixer nozzle testing at the NASA Lewis Aeroacoustic Propulsion Lab [microform] / Gary G. Podboy ... [et al.].

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle [microform] / David W. Lam.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Advanced small rocket chambers option 3 [microform] : 110 1bf Ir-Re rocket / Donald M. Jassowski and Leonard Schoenman.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Development of three-dimensional code for the analysis of jet mixing problem [microform] / Khaled S. Abdol-Hamid.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988-
    • 1988-present

  • 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

  • Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle [microform] : final report / Stephen W.D. Wolf.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Supersonic laminar flow control research [microform] : semiannual report #4, July 1995 - December 1995 / Dr. C.F. Lo, principal investigator.

    • Text
    • Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • A performance comparison of two small rocket nozzles [microform] / Lynn A. Arrington, Brian D. Reed, Angel Rivera, Jr.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Multidisciplinary approach to aerospike nozzle design [microform] / J.J. Korte ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel [microform] : report on the modified D.S.M.A. design / P.S. Barna.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure [microform] / M. Moin Hussaini and John J. Korte.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Combined numerical/analytical perturbation solutions of the Navier-Stokes equations for aerodynamic ejector/mixer nozzle flows [microform] : prepared under grant NGT-51244 / Lawrence Justin De Chant.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Aerodynamic design optimization via reduced Hessian SQP with solution refining [microform] / Dan Feng and Thomas H. Pulliam.

    • Text
    • [Washington, DC] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Supersonic laminar flow control research [microform] : final report, July 1994-June 1996 / C.F. Lo, principal investigator.

    • Text
    • Tullahoma, TN : University of Tennessee, Space Institute ; Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • 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

  • Collective interaction in a linear array of supersonic rectangular jets [microform] : a linear spatial instability study / Jeffrey Hilton Miles.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
    • 1999

  • 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

  • Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle [microform] / Karen A. Deere and Scott C. Asbury.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999

  • Space shuttle ice suppression system validation [microform] : volume II / J.L.F. Porteiro, D.J. Norton, and T.C. Pollock ; prepared by Texas Engineering Experiment Station, Texas A&M University.

    • Text
    • College Station, Tex. : Texas Engineering Experiment Station, Texas A&M University, [1984]
    • 1984

  • Decomposing solid micropropulsion nozzle performance issues [microform] / Brian Reed.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from the NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS55253

  • Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air [microform] / W.I. Scallion.

    • Text
    • Hamtpon, Va. : National Aeronautics and Space Administration, Langley Research Center : [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60070

  • Space shuttle production verification motor-1 (PV-1) static fire. Volume 1 [microform] : final test report / [prepared by Diane Garecht].

    • Text
    • Brigham City, UT : Thiokol Corp., Space Operations ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70072

  • Flight motor set 360L001 (STS-26R) [microform]. Volume 5. Nozzle component : final report / [prepared by Russell J. George].

    • Text
    • Brigham City, UT : Thiokol Corp., Space Operations ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS70022

  • Velocity and temperature decay characteristics of inverted-profile jets [microform] / U. von Glahn, J. Goodykoontz, and C. Wasserbauer.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986

  • Static and dynamic deflection studies of the SRM aft case/nozzle joint [microform] / by David C. Christian, Lawrence D. Kos, and Isaias Torres.

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, Va. : For sale by National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92600

  • Operating characteristics of the multiple critical venturi system and secondary calibration nozzles used for weight-flow measurements in the Langley 16-foot transonic tunnel [microform] / Bobby L. Berrier, Laurence D. Leavitt, and Linda S. Bangert.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS96291

  • Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles [microform] / H.C. Kao, P. L. Burstadt, and A. L. Johns.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration, 1984]
    • 1984

  • 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

  • Free-jet feasibility study of a thermal acoustic shield concept for AST/VCE application [microform] : dual stream nozzles : comprehensive data report / B.A. Janardan, J.F. Brausch, and A.O. Price.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, [1984]
    • 1984

  • Theoretical study on the effect of the design of small (milli-newton) thruster jets on molecular contamination for the space station [microform] / Ben R. Riley, principle investigator.

    • Text
    • Evansville, Ind. : University of Evansville, Dept. of Physics ; [Washington, D.C. : National Aeronautics and Space Administration, 1986]
    • 1986

  • Proposed flight research of a dual-bell rocket nozzle using the NASA F-15 airplane / Daniel S. Jones and Trong T. Bui, Joseph H. Ruf.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50963

  • Lessons learned during TBCC design for the NASA-AFRL joint system study / Christopher A. Snyder, A.M. (Jose) Espinosa.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
    • 2013-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53699

  • Conceptual 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/gpo58350

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