Research Catalog

  • Semi-empirical model for prediction of unsteady forces on an airfoil with application to flutter [microform] / Aparjit J. Mahajan and Krishna Rao V. Kaza.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1992]
    • 1992
  • Aeroelastic stability analyses of two counter rotating propfan designs for a cruise missile model / Aparajit J. Mahajan [and three others].

    • Text
    • Washington, D.C. : NASA, April 1992.
    • 1992-4
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo173618

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