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  • Aerodynamic characteristics and control effectiveness of the HL-20 lifting body configuration at Mach 10 in air [microform] / William I. Scallion.

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

  • Low-speed aerodynamic data for an 0.18-scale model of an F-16XL with various leading-edge modifications [microform] / David E. Hahne.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
    • 1999

  • Conceptual design and analysis of a dynamic scale model of the Space Station Freedom [microform] / D.A. Davis ... [et al.].

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

  • Development of the CSI phase-3 evolutionary model testbed [microform] / M.J. Gronet, D.A. Davis and M.K. Tan.

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

  • Design and construction of a remote piloted flying wing [microform].

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

  • Design and testing of a model CELSS chamber robot [microform].

    • Text
    • [Orlando, Fla.] : University of Central Florida, Mechanical and Aerospace Engineering ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model [microform] / Stacey J. Cotton and Lisa J. Bjarke.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • [The viability of establishing collaborative, reconfigurable research environmentsfor the Human Performance Research Laboratory at NASA Ames [microform] : final technical report, 1987-1992].

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

  • Methods for scaling icing test conditions [microform] / David N. Anderson.

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

  • The velocity and vorticity fields of the turbulent near wake of a circular cylinder [microform] / James Wallace.

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

  • AMC EN-1038 reduced scale solar simulator supplementary test report [microform] / prepared by Robert C. Biering.

    • Text
    • Cleveland, Ohio : Advanced Manufacturing Center, Cleveland State University : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Analysis of advanced solid rocket motor ignition phenomena [microform] : final report / by Winfred A. Foster, Jr., Rhonald M. Jenkins.

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

  • Performance of a miniaturized arcjet [microform] / John M. Sankovic and David T. Jacobson.

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

  • RSRM 10% Scale Model drilled hole plate tests [microform] : final report, contract NAS8-40347 / prepared by ERC, Incorporated, Huntsville Operation.

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

  • Turbulent inflow measurements [microform] : final report, grant number L-1625, period covered: 5 July 1995 to 31 December 1996 / principal investigator, Albert R. George.

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

  • Micromechanical modeling of woven metal matrix composites [microform] : [final contractor report] / Brett A. Bednarcyk and Marek-Jerzy Pindera.

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

  • Azimuthal patterns of the radiated sound field from a turbofan model [microform] / R.H. Thomas ... [et al.].

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
    • 1997

  • Experimental studies in helicopter vertical climb performance [microform] : final report for NASA grant NAG 2-783 / Robert M. McKillip, Jr.

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

  • Analysis of wind tunnel oscillatory data of the X-31A aircraft [microform] / Mark S. Smith.

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

  • Low-power ion thruster development status [microform] / Michael J. Patterson.

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

  • Flow quality measurements in an aerodynamic model of NASA Lewis' Icing Research Tunnel [microform] / Victor A. Canacci and Jose C. Gonsalez.

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

  • Low speed aerodynamics of the X-38 CRV [microform] : summary of research NAG9-927, 5/97-4/98 / Komerath, N.M. ... [et al.].

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

  • Acoustic treatment design scaling methods [microform].

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

  • Comparison of the aerodynamic characteristics of similar models in two size wind tunnels at transonic speeds [microform] / Anthony M. Springer.

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

  • Design and checkout of a high speed research nozzle evaluation rig [microform] / Raymond S. Castner, John D. Wolter.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
    • 1997

  • Atmospheric probe model [microform] : construction and wind tunnel tests : final report : grant no. NCC 2-935 / submitted by Jerald M. Vogel, principal investigator.

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

  • Crashworthy evaluation of a 1/5-scale model composite fuselage concept [microform] / Karen E. Jackson and Edwin L. Fasanella.

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

  • Effects of eddy viscosity on time correlations in large eddy simulation [microform] / Guowei He, R. Rubinstein, Lian-Ping Wang ; prepared for Langley Research Center under contract NAS1-97046.

    • Text
    • Hampton, VA : ICASE, NASA Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
    • 2001

  • A wind tunnel study on the Mars Pathfinder (MPD) lander descent pressure sensor [microform] / J. Francisco Soriano ... [et al.].

    • Text
    • Kennedy Space Center, Fla. : National Aeronautics and Space Administration, John F. Kennedy Space Center ; [Hanover, Md. : NASA Center for AeroSpace Information, 2001]
    • 2001

  • Parametric data from a wind tunnel test on a rocket-based combined-cycle engine inlet [microform] / René Fernandez ... [et al.].

    • 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/LPS26716

  • Testing of densified liquid hydrogen stratification in a scale model propellant tank [microform] / John M. Jurns, Thomas M. Tomsik, William D. Greene.

    • 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/LPS30323

  • Acoustic and laser doppler anemometer results for confluent and 120-lobed E³ mixer exhaust systems for subsonic jet noise reduction [microform] / M. Salikuddin ... [et al.].

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2002]
    • 2002
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS36057

  • Acoustic treatment design scaling methods [microform] : phase II final report / R.E. Kraft ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; ; Hanover, MD : Available from NASA Center for Aerospace Information, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS46998

  • Wind-tunnel evaluation of a 21-percent-scale powered model of a prototype advanced scout helicopter [microform] / Arthur E. Phelps III and John D. Berry.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
    • 1985

  • Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances [microform] / Lisa J. Bjarke.

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59777

  • A reduced model for prediction of thermal and rotational effects on turbine tip clearance [microform] / Javier A. Kypuros, Kevin J. Melcher.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, [2003]
    • 2003
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59607

  • Design and fabrication of the NASA HL-20 full scale research model [microform] / by K. Dean Driver and Robert J. Vess.

    • Text
    • Raleigh, NC : North Carolina State University, Mechnical and Aerospace Engineering, Mars Mission Research Center ; [Hampton, VA : National Aeronautics and Space Administration, Langley Research Center?, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS69902

  • Lobed mixer design for noise suppression [microform] : acoustic and aerodynamic test data analysis / Vinod G. Mengle and Willaim N. Dalton.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Springfield, VA : National Technical Information Service, distributor, [2002-
    • 2002-present
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS71495

  • Preliminary measurement of the noise from the 2/9 scale model of the large-scale advanced propfan (LAP) propeller, SR-7A [microform] / James H. Dittmar.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1985]
    • 1985

  • SRB/FWC water impact [microform] : flexible body loads test / prepared by Bolt Beranek and Newman Inc. ; prepared for George C. Marshall Space Flight Center.

    • Text
    • Marshall Space Flight Center, AL : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1984]
    • 1984

  • Evaluation of the feasibility of scale modeling to quantify wind and terrain effects on low-angle sound propagation [microform] / G.S. Anderson, ... [et al.].

    • Text
    • Cambridge, MA : Bolt, Beranek and Newman, Inc. ; Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS88247

  • Ares I Scale Model Acoustic Test overpressure results / M.J. Casiano, D.A. Alvord, and D.M. McDaniels.

    • Text
    • Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, [2011]
    • 2011
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo24420

  • Initial investigation of the acoustics of a counter-rotating open rotor model with historical baseline blades in a low-speed wind tunnel / David M. Elliott.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo26275

  • Aerodynamic effects of simulated ice accretion on a generic transport model / Andy P. Broeren ... [and others].

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo26345

  • Further evaluation of scaling methods for rotorcraft icing / Jen-Ching Tsao, Richard E. Kreeger.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo30594

  • Ice-accretion scaling using water-film thickness parameters / David N. Anderson, Alejandro Feo.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, [2003]
    • 2003
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo33286

  • Ice-accretion scaling using water-film thickness parameters [microform] / David N. Anderson, Alejandro Feo.

    • Text
    • [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center, [2003]
    • 2003

  • Evaluation of icing scaling on swept NACA 0012 airfoil models / Jen-Ching Tsao, Sam Lee.

    • Text
    • Brook Park, Ohio : Ohio Aerospace Institute ; Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, May 2012.
    • 2012-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo32879

  • Experimental investigation of shock-cell noise reduction for dual-stream nozzles in simulated flight : comprehensive data report / K. Yamamoto [and four others].

    • Text
    • Cincinnati, Ohio : General Electric Company, Aircraft Engine Business Group, February, 1984.
    • 1984-2
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo58844

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