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  • Some observations on the Houbolt-Rainey and peak-hold methods of flutter onset prediction [microform] / Robert V. Doggett, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1989

  • A preliminary look at techniques used to obtain airdata from flight at high angles of attack [microform] / Timothy R. Moes and Stephen A. Whitmore.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Pressure distributions from subsonic tests of a NACA 0012 semispan wing model [microform] / Zachary T. Applin.

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

  • 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

  • Motion of the heliospheric termination shock at high heliographic latitude [microform] / Aaron Barnes.

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

  • Experimental investigation of unsteady shock wave turbulent boundary layer interactions about a blunt fin [microform] / by Paul J. Barnhart and Isaac Greber.

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

  • Summary report of the orbital X-34 wing static aeroelastic study [microform] / Ramadas K. Prabhu ; prepared ... under contract NAS1-96014.

    • Text
    • Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

  • Demodulation system for fiber optic Bragg grating dynamic pressure sensing [microform] / John D. Lekki, Grigory Adamovsky, Bertram Floyd.

    • 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/LPS23305

  • 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

  • Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel [microform] / David M. Schuster.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
    • 2001
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS22955

  • Method for experimental determination of flutter speed by parameter identification [microform] / E. Nissim and Glenn B. Gilyard.

    • 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, 1989.
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60135

  • The infinite line pressure probe [microform] / David R. Englund and W. Bruce Richards.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS99073

  • Real-time pilot guidance system for improved flight test maneuvers [microform] / Robert R. Meyer, Jr. and Edward T. Schneider.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1984.
    • 1984

  • A technique for dynamically calibrating transducers at cryogenic temperatures [microform] / Barry V. Gibbens.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1983]
    • 1983
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS100805

  • Data driven model development for the supersonic semispan transport (S⁴T) / Sunil L. Kukreja.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24465

  • A data base and analysis program for shuttle main engine dynamic pressure measurements : final report / by Thomas Coffin.

    • Text
    • [Huntsville, Ala.] : Wyle Laboratories Scientific Services & Systems Group ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24526

  • A data base and analysis program for shuttle main engine dynamic pressure measurements [microform] : final report / by Thomas Coffin.

    • Text
    • [Huntsville, Ala.] : Wyle Laboratories Scientific Services & Systems Group ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1986]
    • 1986

  • Flight test results from the rake airflow gage experiment on the F-15B airplane / Michael A. Frederick and Nalin A. Ratnayake.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo30629

  • Active combustion control for aircraft gas-turbine engines : experimental results for an advanced, low-emissions combustor prototype / John C. DeLaat ... [and others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo31847

  • Aeroelastic analyses of the SemiSpan Supersonic Transport (S⁴T) wind tunnel model at Mach 0.95 / Jiyoung Hur.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2014.
    • 2013-7
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo53309

  • Mars entry atmospheric data system modeling, calibration, and error analysis / Christopher D. Karlgaard [and four others].

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55644

  • Acoustic database for turbofan engine core-noise sources, volume I, final report / Grant Gordon.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
    • 2015-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65194

  • Experimental verification of buffet calculation procedure using unsteady PSP / Jayanta Panda.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo67582

  • Assessment of JVX proprotor performance data in hover and airplane-mode flight conditions / C.W. Acree, Jr.

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2016.
    • 2016-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo68686

  • An investigation of surge in a high-speed centrifugal compressor using digital PIV / Mark P. Wernet and Michelle M. Bright, Gary J. Skoch.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2002.
    • 2002-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS43729

  • Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel / David M. Schuster.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2001.
    • 2001-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS22955

  • An investigation of the causes of failure of flexible thermal protection materials in an aerodynamic environment / Charles F. Coe.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Ames Research Center, March 1987.
    • 1987-3

  • Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique / Gary E. Erickson.

    • Text
    • Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, [2013]
    • 2013
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo40579

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