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  • Increased heat transfer to a cylindrical leading edge due to spanwise variations in the freestream velocity [microform] / D.L. Rigby and G.J. Van Fossen

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
    • 1991

  • An implementation of a chemical and thermal nonequilibrium flow solver on unstructured meshes and application to blunt bodies [microform] / Ramadas K. Prabhu.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1994]
    • 1994

  • Adjustable bias column end joint assembly [microform] / inventor, Richard E. Walsom, Harold G. Bush.

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

  • Slow wave vane structure with elliptical cross-section slots, an analysis [microform] / Henry G. Kosmahl.

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

  • Numerical mixing calculations of confined reacting jet flows in a cylindrical duct [microform] / Victor L. Oechsle, J.D. Holdeman.

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

  • Field and data analysis studies related to the atmospheric environment : final report of work performed under NAS8-39776, for the period, 21 February 1991 - 1 March 1994 [microform] / Stanley Kidder ... [et al.].

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

  • Dynamic and thermal response finite element models of multi-body space structural configurations [microform] / Harold H. Edighoffer.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1987]
    • 1987

  • An analytical study of the effects of transverse shear deformation and anisotropy on natural vibration frequencies of laminated cylinders [microform] / Dawn C. Jegley.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1988]
    • 1988

  • Analytic solutions of the vector Burgers' equation [microform] / by Steven Nerney, Edward J. Schmahl, and Z.E. Musielak.

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

  • Experimental study of vortex breakdown in a cylindrical, swirling flow [microform] / J.L. Stevens ... [et al.].

    • Text
    • [Stanford, Calif.] : Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center : Joint Institute for Aeronautics and Acoustics, Stanford University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Technical characteristics of a novel helical-groove traveling-wave tube structure [microform] / Thomas M. Wallett ... [et al.].

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

  • A study of failure in small pressurized cylindrical shells containing a crack [microform] / Craig A. Barwell, Lorenz Eber, and Ian M. Fyfe.

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

  • HOTCFGM-1D [microform] : a coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures / Marek-Jerzy Pindera, Jacob Aboudi.

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

  • Free vibration of fiber composite thin shells in a hot environment [microform] / Pascal K. Gotsis and James D. Guptill.

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

  • Impact of functionally graded cylinders [microform] : theory / Jacob Aboudi, Marek-Jerzy Pindera.

    • 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/LPS22681

  • Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius [microform] Thomas J. Horn, Amanie N. Abdelmessih.

    • Text
    • Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2000]
    • 2000
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS31291

  • Flow separation in shock wave boundary layer interactions at hypersonic speeds [microform] / A. Hamed.

    • 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, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS61576

  • Controlled crack growth specimen for brittle systems [microform] / Anthony M. Calomino and David N. Brewer.

    • Text
    • [Washington, D.C.] : NASA ; [St. Louis, Mo.] : US Army Aviation Systems Command ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
    • 1990
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS68912

  • Rotating reactor studies [microform] : final report RAI-89-RR-2 / prepared by Glyn O. Roberts.

    • Text
    • Vienna, VA : Roberts Associates, Inc. ; MSFC, AL : George C. Marshall Space Flight Center, [1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS64318

  • Heat transfer distributions around nominal ice accretion shapes formed on a cylinder in the NASA Lewis icing research tunnel [microform] / G. J. Van Fossen, ... [et al.].

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

    Available Online

    http://purl.access.gpo.gov/GPO/LPS98924

  • A critical evaluation of various methods for the analysis of flow-solid interaction in a nest of thin cylinders subjected to cross flows : interim report / by Sang-Wook Kim.

    • Text
    • Marshall Space Flight Center, Ala. : NASA-Marshall Space Flight Center, Systems Dynamics Laboratory, Science and Engineering Directorate, [1987]
    • 1987
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo25784

  • A critical evaluation of various methods for the analysis of flow-solid interaction in a nest of thin cylinders subjected to cross flows [microform] : interim report / by Sang-Wook Kim.

    • Text
    • Marshall Space Flight Center, Ala. : NASA-Marshall Space Flight Center, Systems Dynamics Laboratory, Science and Engineering Directorate, [1987]
    • 1987

  • Validation of the predicted circumferential and radial mode sound power levels in the inlet and exhaust ducts of a fan ingesting distorted inflow / L. Danielle Koch.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo26304

  • Application of advanced nondestructive evaluation techniques for cylindrical composite test samples / Richard E. Martin, Donald J. Roth and Jonathan A. Salem.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
    • 2013-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo47604

  • Buckling design and analysis of a payload fairing 1/6th cylindrical arc-segment panel / Daniel N. Kosareo, Stanley T. Oliver, Brett A. Bednarcyk.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2013.
    • 2013-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52886

  • Effect of roller geometry on roller bearing load-life relation / Fred B. Oswald and Erwin V. Zaretsky, Joseph V. Poplawski.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2015.
    • 2015-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo65867

  • Experimental and numerical characterization of a steady-state cylindrical blackbody cavity at 1100 degrees celsius / Thomas J. Horn, Amanie N. Abdelmessih.

    • Text
    • Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, August 2000.
    • 2000-8
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS31291

  • Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes / Percy J. Bobbitt [and four others].

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, 2012.
    • 2012
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo37677

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