Research Catalog

  • Experimental methods of hypersonics [by] J. Lukasiewicz.

    • Text
    • New York, M. Dekker, 1973.
    • 1973
    • 1 Item
    FormatCall NumberItem Location
    Text JSE 74-70Offsite
  • Advanced experimental techniques for study of hypervelocity flight.

    • Text
    • [Denver?]
    • 19-19
    • 2 Items
    FormatCall NumberItem Location
    Text JSP 74-250 4th (1965)Offsite
    FormatCall NumberItem Location
    Text JSP 74-250 5th, v. 1 (1967)Offsite
  • Experimentelle und theoretische Untersuchungen von turbulenten Grenzschichten bei Uberschallströmung. [Von] H[ans] U[lrich] Meier.)

    • Text
    • Göttingen (Max-Planck-Institut f. Strömungsforschung; Aerodynamische Versuchsanstalt) 1970.
    • 1970
    • 1 Item
    FormatCall NumberItem Location
    Text JSK 74-4 Nr. 49 Nr. 49-53Offsite
  • Advances in hypervelocity techniques; proceedings. Edited by Arthur M. Krill. Sponsored by University of Denver, Denver Research Institute, 20 and 21 March 1962.

    • Text
    • New York, Distributed by Plenum Press [1962]
    • 1962
    • 1 Item
    FormatCall NumberItem Location
    Text PCP (Symposium on Hypervelocity Techniques. 2d, Denver, 1962. Advances in hypervelocity techniques) (1962)Offsite
  • Langley 8-ft. HTT test 139 gas analyses [microform] / Danny R. Sprinkle and Patricia P. Davis.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows [microform] / Robert L. McKenzie and Douglas G. Fletcher.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992
  • A System to measure flow moisture content in hypersonic wind tunnels [microform] / James W. West.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992
  • Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel [microform] / S. Venkateswaran, L. Roane Hunt, Ramadas K. Prabhu.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1992.
    • 1992
  • Real gas flow parameters for NASA Langley 22-inch Mach 20 helium tunnel [microform] / Brian R. Hollis.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
    • 1992
  • MACH 6 electroformed nickel nozzle refurbishment ; FNAS investigation of ultra-smooth surfaces [microform] / Robert Rood ... [et al.].

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992
  • Mach 5 electroformed nickel nozzle refurbishment [microform] : FNAS investigation of ultra-smooth surfaces / Robert Rood, Charles Griffith and Darell Engelhaupt.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992
  • Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation [microform] / Lawrence D. Huebner, Marc W. Kniskern, William J. Monta.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993
  • Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel [microform] : final report for NAG-1-767 / principal investigators: Jale F. Akyurtlu, co-principal investigator: Ates F. Akyurtlu.

    • Text
    • [Hampton, Va.] : Hampton University, Dept. of Engineering ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1993
  • Enhancing U.S. competitiveness : NASA hypersonics research and wind tunnel programs : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, second session, March 15, 1994.

    • Text
    • Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1994.
    • 1994
  • Nonintrusive fast response oxygen monitoring system for high temperature flows [microform] / Daniel B. Oh and Alan C. Stanton.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
    • 1993
  • An assessment of laser velocimetry in hypersonic flow [microform] : final report.

    • Text
    • Palo Alto, CA : Complere, Inc. ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
    • 1992
  • Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel [microform] : status report, October 31, 1991 / investigators, Jale F. Akyurtlu (pi), Ates F. Akyurtlu (co-pi).

    • Text
    • [Hampton, Va.] : Hampton University, Dept. of Engineering ; [Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991
  • Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 [microform] / Scott D. Holland.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
  • Operating capability and current status of the reactivated NASA Lewis Research Center hypersonic tunnel facility [microform] / Scott R. Thomas, Charles J. Trefny, and William D. Pack.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995?]
    • 1995
  • Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing [microform] / D.E. Reubush, R.L. Puster, H.N. Kelly.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1987]
    • 1987
  • Support of the eight-foot high temperature tunnel modification project [microform] : final report for the period ended August 16, 1987 / by Kim Chi Ngo and Roland R. Mielke, principal investigator.

    • Text
    • Norfolk, Va. : Dept. of Electrical and Computer Engineering, College of Engineering and Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Magnetohydrodynamics Accelerator Research into Advanced Hypersonics (MARIAH) [microform] : final report / Jack A. Baughman ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service [distributor, 1997]
    • 1997
  • Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF [microform] / H. Douglas Perkins, Scott R. Thomas, and William D. Pack.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996
  • Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly [microform] / Gregory J. Brauckmann; John W. Paulson, Jr.; K. James Weilmuenster.

    • Text
    • Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995
  • Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms [microform] / Nathan S. Jacobson.

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    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
    • 1999
  • 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
  • Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels [microform] / Gregory M. Buck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1995]
    • 1995
  • 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.

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    • Houston, Tex. : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.
    • 1985
  • Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) [microform] / by John Marroquin.

    • Text
    • Houston, Tex. : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.
    • 1985
  • Pursuit of Power : NASA's Propulsion Systems Laboratory, No. 1 & 2 / Robert S. Arrighi.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, NASA History Division, Office of External Relations, 2012.
    • 2012
    • 1 Item

    Available Online

    http://purl.fdlp.gov/GPO/gpo49549
    FormatCall NumberItem Location
    Text JBF 18-558Schwarzman Building - General Research Room 315

    Available - Can be used on site. Please visit New York Public Library - Schwarzman Building to submit a request in person.

  • Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF / H. Douglas Perkins, Scott R. Thomas, and William D. Pack.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.
    • 1996-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo70728
  • Experimental investigation of roughness effects on transition onset and turbulent heating augmentation on a hemisphere at Mach 6 and Mach 10 / Brian R. Hollis.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 2017.
    • 2017-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo82540
  • Quantitative global heat transfer in a Mach-6 quiet tunnel / John P. Sullivan [and ten others].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32903
  • Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle.

    • Text
    • [Paris] North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1959.
    • 1959
    • 1 Item
    FormatCall NumberItem Location
    Text 92519.841Off-site
  • Advances in hypervelocity techniques; proceedings. Edited by Arthur M. Krill. Sponsored by University of Denver, Denver Research Institute, 20 and 21 March 1962.

    • Text
    • New York, Distributed by Plenum Press [1962]
    • 1962
    • 1 Item
    FormatCall NumberItem Location
    Text 92514.8918Off-site
  • A study of the feasibility of a hypersonic tunnel using a weakly ionized gas.

    • Text
    • 1968.
    • 1968
    • 1 Item
    FormatCall NumberItem Location
    Text PRIN 6848 1968 .683Off-site
  • The hypersonic facility of the Polytechnic Institute of Brooklyn and its application to problems of hypersonic flight, by Antonio Ferri and Paul A. Libby.

    • Text
    • [Paris, North Atlantic Treaty Organization, 1957]
    • 1957
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-136Off-site
  • The light gas hypersonic gun tunnel at A.R.D.E., Fort Halstead, Kent / by R. N. Cox and D. F. T. Winter.

    • Text
    • Paris : North Atlantic Treaty Organization, 1957.
    • 1957
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-139Off-site
  • Hypersonic shock tube equipment at the National Physical Laboratory, U. K. / by D. L. Schultz and B. D. Henshall.

    • Text
    • Paris : North Atlantic Treaty Organization, 1957.
    • 1957
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-147Off-site
  • A summary of design techniques for axisymmetric hypersonic wind tunnels.

    • Text
    • [Paris] North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1958.
    • 1958
    • 1 Item
    FormatCall NumberItem Location
    Text AGARDOGRAPH-35Off-site
  • Development of the spark-heated, hypervelocity, blowdown tunnel-hotshot / by R.W. Perry and W.N. MacDermott.

    • Text
    • Paris : North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1958.
    • 1958
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-233Off-site
  • Pursuit of Power : NASA's Propulsion Systems Laboratory, No. 1 & 2 / Robert S. Arrighi.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, NASA History Division, Office of External Relations, 2012.
    • 2012
    • 1 Item
    FormatCall NumberItem Location
    Text TL568.P75 A77 2012Off-site
  • Advances in hypervelocity techniques; proceedings. Edited by Arthur M. Krill. Sponsored by University of Denver, Denver Research Institute, 20 and 21 March 1962.

    • Text
    • New York, Distributed by Plenum Press [1962]
    • 1962
    • 1 Item
    FormatCall NumberItem Location
    Text 92514.8918Off-site
  • The light gas hypersonic gun tunnel at A.R.D.E., Fort Halstead, Kent / by R. N. Cox and D. F. T. Winter.

    • Text
    • Paris : North Atlantic Treaty Organization, 1957.
    • 1957
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-139Off-site
  • Hypersonic shock tube equipment at the National Physical Laboratory, U. K. / by D. L. Schultz and B. D. Henshall.

    • Text
    • Paris : North Atlantic Treaty Organization, 1957.
    • 1957
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-147Off-site
  • A summary of design techniques for axisymmetric hypersonic wind tunnels.

    • Text
    • [Paris] North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development, 1958.
    • 1958
    • 1 Item
    FormatCall NumberItem Location
    Text AGARDOGRAPH-35Off-site
  • Pursuit of Power : NASA's Propulsion Systems Laboratory, No. 1 & 2 / Robert S. Arrighi.

    • Text
    • Washington, DC : National Aeronautics and Space Administration, NASA History Division, Office of External Relations, 2012.
    • 2012
    • 1 Item
    FormatCall NumberItem Location
    Text TL568.P75 A77 2012Off-site

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