Research Catalog

  • Interaction entre une onde de choc oblique et une grille d'aubes fixes parcourues par un écoulement subsonique : contribution à l'étude des propagations d'ondes instationnaires dans un étage de compresseur supersonique / von Daniel Favrat.

    • Text
    • Zürich : Juris-Verlag, [1977]
    • 1977
    • 1 Item
    FormatCall NumberItem Location
    Text JSK 76-354 no. 1-4Offsite
  • Supersonic propulsion simulation by incorporating component models in the Large Pertubation Inlet (LAPIN) computer code [microform] / Gary L. Cole and Jacques C. Richard.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration, [1991]
    • 1991
  • Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations [microform] : final technical report / Miklos Sajben, Donald D. Freund.

    • Text
    • [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
    • 1998
  • Mass balancing of hollow fan blades [microform] / Robert E. Kielb.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986
  • Analysis of fully stalled compressor [microform] / Wojciech Rostafinski.

    • Text
    • [Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, 1986]
    • 1986
  • Advanced compressors.

    • Text
    • [Neuilly-sur-Seine, 1970]
    • 1970
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-LS-39-70Off-site

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