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  • Formation of asymmetric separated flow past slender bodies of revolution at large angles of attack [microform].

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

  • Vortex systems on slender rotating bodies and their effect on the aerodynamic coefficients [microform] / M. Fiechter.

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

  • The pratical calculation of the aerodynamic characteristics of slender finned vehicles [microform] / by James S. Barrowman.

    • Text
    • Washington, D.C. : [National Aeronautics and Space Administration, 1967]
    • 1967

  • Large-deformation displacement transfer functions for shape predictions of highly flexible slender aerospace structures / William L. Ko and Van Tran Fleischer.

    • Text
    • Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, December 2013.
    • 2013-12
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo55847

  • The practical calculation of the aerodynamic characteristics of slender finned vehicles / by James S. Barrowman.

    • Text
    • Washington, D.C. : [National Aeronautics and Space Administration], March 1967.
    • 1967-3
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/LPS68628

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