Research Catalog

New! Try our Article Search to discover online journals, books, and more from home with your library card.

Selected filters.Clear Filters

  • Interlaminar stress analysis of dropped-ply laminated plates and shells by a mixed method [microform] / Peter N. Harrison, Eric R. Johnson, James H. Starnes.

    • Text
    • Blacksburg, Va. : Virginia Polytechnic Institute and State University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
    • 1994

  • Application of viscous-inviscid interaction methods to transonic turbulent flows [microform] / by D. Lee, R.H. Pletcher.

    • Text
    • [Ames, Iowa] : Iowa State University. Engineering Research Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Stability limits and dynamics of nonaxisymmetric liquid bridges [microform] : final report / prepared by J. Iwan D. Alexander, principal investigator.

    • Text
    • Huntsville, AL : Center for Microgravity and Materials Research, University of Alabama in Huntsville ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies [microform] / Irina G. Brykina, Carl D. Scott.

    • Text
    • Houston, Tex. : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998

  • Parametric fin-body and fin-plate database for a series of 12 missile fins [microform] / Jerry M. Allen.

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

  • The unsteady laminar boundary layer on an axisymmetric body subject to small amplitude fluctuations in the free-stream velocity [microform] / Peter W. Duck.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]
    • 1991
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS59768

  • An experimental investigation of the impingement of a planar shock wave on an axisymmetric body at Mach 3 [microform] / A. Brosh and M. I. Kussoy.

    • Text
    • Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
    • 1983

  • An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [microform] / Dorothy G. Arbiter.

    • Text
    • Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1985]
    • 1985

  • An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies / Irina G. Brykina, Carl D. Scott.

    • Text
    • Houston, Texas : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, May 1998.
    • 1998-5
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo83038

  • Parametric fin-body and fin-plate database for a series of 12 missile fins / Jerry M. Allen.

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

    Available Online

    https://purl.fdlp.gov/GPO/LPS70083

No results found from Digital Research Books Beta

Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.

digital-research-book
Explore Digital Research Books Beta