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  • Entwicklung von Plasmabrennern für Luftbetrieb zum Einsatz in Raumfahrt-Versuchsanlagen. Von R. Gebel. Mit 117 Abb.

    • Text
    • (München, Zentralstelle f. Luftfahrtdokumentation u. -information) 1969.
    • 1969
    • 1 Item
    FormatCall NumberItem Location
    Text JSG 81-1Offsite

  • The Peenemünde wind tunnels : a memoir / Peter P. Wegener.

    • Text
    • New Haven : Yale University Press, c1996.
    • 1996
    • 1 Item
    FormatCall NumberItem Location
    Text JSE 96-1275Offsite

  • High-speed wind tunnel testing [by] Alan Pope [and] Kennith L. Goin.

    • Text
    • New York, Wiley [1965]
    • 1965
    • 1 Item
    FormatCall NumberItem Location
    Text VDY (Pope, A. High speed wind tunnel testing)Offsite

  • Engine component instrumentation development facility at NASA Lewis Research Center [microform] / Robert J. Bruckner, Alvin E. Buggele, and Jan Lepicovsky.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

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

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va.? : National Technical Information Service, distributor, 1992]
    • 1992

  • Flow quality studies of the NASA Lewis Research Center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel [microform] / E. Allen Arrington and Mark T. Pickett.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

  • User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel [microform] / Ronald H. Soeder.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992

  • Results of a FRSI material test under Space Shuttle ascent conditions in the Ames Research Center SX7 foot supersonic wind tunnel [microform] / by P.L. Lemoine, J.G.R. Collette.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992

  • NASA Lewis 8- by 6-foot supersonic wind tunnel user manual [microform] / Ronald H. Soeder.

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

  • CNSFV code development, virtual zone Navier-Stokes computations of oscillating control surfaces and computational support of the laminar flow supersonic wind tunnel [microform] / Goetz H. Knopfler.

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

  • Method of characteristics design of a supersonic wind tunnel nozzle with square cross-section [microform] : status report for NASA Langley grant NAG-1-113, supplement 3 / principal investigator: Steven P. Schneider.

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

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

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va.? : National Technical Information Service, distributor, 1992]
    • 1993

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

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration : National Technical Information Service, distributor, 1991]
    • 1991

  • Improved pressure measurement system for calibration of the NASA LeRC 10x10 supersonic wind tunnel [microform] / Philip Z. Blumenthal andStephen M. Helland.

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

  • NASA Lewis wind tunnel model systems criteria [microform] / Ronald H. Soeder and Henry C. Haller.

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

  • A supersonic tunnel for laser and flow-seeding techniques [microform] / Robert J. Bruckner and Jan Lepicovsky.

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

  • Review of aeronautical wind tunnel facilities [microform] / Committee on Assessment of National Aeronautical Wind Tunnel Facilities, Aeronautics and Space Engineering Board, Commission on Engineering and Technical Systems, National Research Council.

    • Text
    • Washington, D.C. : National Academy Press ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Simulation of pressure and temperature responses for the 20 inch supersonic wind tunnel [microform] / Mark A. Motter.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Wind-tunnel results of advanced high-speed propellers at takeoff, climb, and landing Mach numbers [microform] / George L. Stefko and Robert J. Jeracki.

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

  • Improved speed control system for an 87,000 hp wind tunnel drive [microform] / Edward A. Becks, Timothy J. Bencic, Philip Z. Blumenthal.

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

  • Supersonic laminar flow control research [microform] : semi-annual report #2, July 1994 - December 1994 / C.F. Lo, principal investigator.

    • Text
    • Moffett Field, CA : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • 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

  • Supersonic laminar flow control research [microform] : semiannual report #2 / Dr. C.F. Lo, principal investigator.

    • Text
    • Moffett Field, Calif. : Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Computational support of the lamimar [i.e. laminar] supersonic wind tunnel, CNSFV code development, Maglev, and grid generation [microform] / Goetz H. Klopfer.

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

  • Supersonic quiet-tunnel development for laminar-turbulent transition research [microform] : final report for NASA Langley grant NAG-1-1607 / Steven P. Schneider.

    • Text
    • [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

  • Design and testing of an oblique all-wing supersonic transport [microform] / Christopher A. Lee.

    • Text
    • San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • User manual for NASA Lewis 10- by 10-foot supersonic wind tunnel [microform] / Ronald H. Soeder.

    • Text
    • [Washington, DC] : 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 / C.F. Lo, principal investigator.

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

  • Instantaneous flow measurements in a supersonic wind tunnel using spectrally resolved Rayleigh scattering [microform] / Richard G. Seasholtz, Alvin E. Buggele, and Mark F. Reeder.

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

  • NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10̊ cone at Mach 1.6 [microform] / Stephen W.D. Wolf, James A. Laub.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • An experimental device for generating high frequency perturbations in supersonic wind tunnels [microform] / Kevin J. Melcher and Mounir B. Ibrahim.

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

  • Low speed calibration of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1995 test) [microform] : under contract NAS3-27186 / E. Allen Arrington and Jose C. Gonsalez.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Baseline calibration of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1991 and 1992 tests) [microform] / E. Allen Arrington, Mark T. Pickett and Ronald H. Soeder.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, Va. : National Technical Information Service, distributor, [1998]
    • 1998

  • Flow quality and operational enhancements in the NASA Lewis 8- by 6-Foot Supersonic Wind Tunnel [microform] / E. Allen Arrington, Jose C. Gonsalez, and Edward A. Becks.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Subsonic flow quality surveys of the NASA Lewis Research Center 10- by 10-foot supersonic wind tunnel [microform] / E. Allen Arrington and Jose C. Gonsalez.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service [distributor, 1998]
    • 1998

  • Flow field surveys of the NASA Lewis Research Center 8- by 6-foot supersonic wind tunnel (1993 test) [microform] / E. Allen Arrington.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service [distributor, 1998]
    • 1998

  • Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21) [microform] / A.M. Springer.

    • Text
    • [Huntsville, Ala.] : National Aeronautics and Space Administration, Marshall Space Flight Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
    • 1998

  • NASA Glenn 1-by 1-foot supersonic wind tunnel user manual [microform] / Kirk D. Seablom ... [et al.].

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

  • Pressure probe designs for dynamic pressure measurements in a supersonic flow field [microform] / A. Robert Porro.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS23204

  • Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C) [microform] / J. Marroquin.

    • Text
    • Houston, Tex. : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.
    • 1985

  • Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data [microform] / D.R. Reddy and T.J. Benson and L.J. Weir ; prepared for the 28th Aerospace Sciences Meeting sponsored by the American Society of Aeronautics and Astronautics, Reno, Nevada, January 8-11, 1990.

    • Text
    • [Washington, D.C.] : NASA ; Springfield, Va. : For sale by the National Technical Information Service, [1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69416

  • Current wind tunnel capability and planned improvements at Lewis Research Center [microform] / David N. Bowditch.

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

  • Laminarization of a boundary layer in a supersonic nozzle by cooling of the surface [microform] / V.P. Maksimov and A.A. Maslov.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, [1983]
    • 1983

  • Calibration of the NASA Glenn 8- by 6-foot supersonic wind tunnel (1996 and 1997 tests) / E. Allen Arrington.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo27462

  • Analysis of buzz in a supersonic inlet / Rodrick V. Chima.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30597

  • Wind tunnel testing of a one-dimensional laser beam scanning and laser sheet approach to shock sensing / Roger Tokars ... [and others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32157

  • Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design / Randy Thomas and Thomas J. Stueber.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2013.
    • 2013-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo49566

  • Investigation of materials for boundary layer control in a supersonic wind tunnel / Alexander C. Braafladt, John M. Lucero and Stefanie M. Hirt.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2013.
    • 2013-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo50546

  • Background pressure profiles for sonic boom vehicle testing in the NASA Glenn 8- by 6-foot supersonic wind tunnel / Raymond Castner [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, July 2013.
    • 2013-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53006

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