Research Catalog

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  • Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels [microform] / William L. Ko and Raymond H. Jackson.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
    • 1991

  • Detailed near-wake flowfield surveys with comparison to an Euler method of an aspect ratio 4 rectangular wing [microform] / M.D. Klinge, S.O. Kjelgaard and J.N. Perkins.

    • Text
    • [Washington, D.C. : National Aeronautics and Space Administration : Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987

  • The effect of aspect ratio and fluid flow on crystal growth [microform] : second semi-annual report / by Patrick G. Barber.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Effect of aspect ratio on sidewall boundary-layer influence in two-dimensional airfoil testing [microform] / A.V. Murthy.

    • Text
    • Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service, distributor], 1986.
    • 1986

  • Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊ [microform] / Scott P. Fears, Holly M. Ross, and Thomas M. Moul.

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

  • An aspect ratio bound for triangulating a d-grid cut by a hyperplane [microform] / Scott A. Mitchell, Stephen A. Vavasis.

    • Text
    • [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • 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

  • Sensitivity analysis of flutter response of a wing incorporating finite-span corrections [microform] / Jason C. Issac, Rakesh K. Kapania, and J.-F. M. Barthelemy.

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

  • Buckling and postbuckling behavior of laminated composite plates with a cutout [microform] / Michael P. Nemeth.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • A comparison of structurally connected and multiple spacecraft interferometers [microform] / Derek M. Surka and Edward F. Crawley.

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

  • Joint research effort on vibrations of twisted plates [microform] : phase 1, final results / Robert E. Kielb, ... [et al.].

    • 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

  • Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods [microform] / William L. Ko.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : Available from the National Technical Information Service, 1995]
    • 1995
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS60789

  • Flow-field surveys for rectangular nozzles / K. B. M. Q. Zaman.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo28432

  • Acoustic measurements of rectangular nozzles with bevel / James E. Bridges.

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

    Available Online

    https://purl.fdlp.gov/GPO/gpo32083

  • Comparison of high aspect ratio cooling channel designs for a rocket combustion chamber with development of an optimized design / by Mary F. Wadel.

    • Text
    • Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1998.
    • 1998-1
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo174895

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