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  • 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

  • Uncertainty analysis of inertial model attitude sensor calibration and application with a recommended new calibration method [microform] / John S. Tripp and Ping Tcheng.

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

  • Experimental uncertainty and drag measurements in the National Transonic facility [microform] / Stephen M. Batill.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Overview of the 1989 Wind Tunnel Calibration Workshop [microform] / Arthur Henderson Jr., L. Wayne McKinney.

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

  • The NASA Langley 8-foot transonic pressure tunnel calibration [microform] / Cuyler W. Brooks, Charles D. Harris, and Patricia G. Reagon.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Correlation of transonic-cone Preston-tube data and skin friction [microform] : final report (research grant number NAG 2-76) (Nov. 80 - May 84) / prepared by A. S. Abu-Mostafa and T.D. Reed.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984

  • Flow quality improvements in the NASA Lewis Research Center 9- by 15-foot low speed 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, 1995]
    • 1995

  • Rapid calibration of seven-hole probes [microform] / A.L. Ericksen ... [et al.].

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

  • A longitudinal aerodynamic data repeatability study for a commercial transport model test in the National Transonic Facility [microform] / R.A. Wahls ... [et al.].

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

  • The new heavy gas testing capability in the NASA Langley Transonic Dynamics Tunnel [microform] / Stanley R. Cole, José A. Rivera, Jr.

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

  • Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test) [microform] / E. Allen Arrington and Jose C. Gonsalez.

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

  • Calibration of NASA Lewis Research Center 9- by 15-Foot low speed wind tunnel (1992 text) [microform] / E. Allen Arrington, and Mark T. Pickett and Ronald H. Soeder.

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

  • Aerodynamic calibration of the NASA Lewis icing research tunnel (1997 tests) [microform] / Jose C. Gonsalez and E. Allen Arrington ; prepared for the 36th Aerospace Sciences Meeting and Exhibit ; sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 12-15, 1998.

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

  • The NASA Langley 16-foot transonic tunnel [microform] : historical overview, facility description, calibration, flow characteristics, and test capabilities / Francis J. Capone ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS54050

  • Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall [microform] / Joel L. Everhart and Percy J. Bobbitt.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60769

  • Flow unsteadiness effects on boundary layers [microform] / by Sreedhara V. Murthy.

    • Text
    • [Moffett Field, Calif. : NASA Ames Research Center, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60942

  • Langley mach 4 scramjet test facility [microform] / Earl H. Andrews, Jr. ... [et al.].

    • 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/LPS96480

  • NASA Glenn icing research tunnel : 2014 cloud calibration procedure and results / Judith F. Van Zante [and three others].

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2014.
    • 2014-10
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo57996

  • A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel / Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
    • 1980-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo71172

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