Research Catalog

  • Zur experimentellen Prüfung instationärer dreidimensionaler Tragflächentheorien bei inkompressibler Strömung.

    • Text
    • Göttingen (Max-Planck-Institut für Strömungsforschung und Aerodynamische Versuchsanstalt) 1967.
    • 1967
    • 1 Item
    FormatCall NumberItem Location
    Text PAA (Max-Planck-Institut für Strömungsforschung, Göttingen. Mitteilungen. v. 36-40 (1966-67)Offsite
  • Development and application of a program to calculate transonic flow around an oscillating three-dimensional wing using finite difference procedures [microform] Warren H. Weatherhill, F. Edward Ehlers.

    • Text
    • [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
    • 1989
  • The NYU inverse swept wing code [microform] / F. Bauer, P. Garabedian, and G. McFadden.

    • Text
    • New York, N.Y. : Courant Institute of Mathematical Sciences, New York University ; [Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : National Technical Information Service, distributor, 1983]
    • 1983
  • Development and application of algorithms for calculating the transonic flow about harmonically oscillating wings [microform] / F. Edward Ehlers, Warren H. Weatherhill, and Elizabeth L. Yip.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1984]
    • 1984
  • AGARD standard aeroelastic configurations for dynamic response [microform] : candidate configuration I.-wing 445.6 / E. Carson Yates, Jr.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1987]
    • 1987
  • Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment [microform] / James T. Howlett and Samuel R. Bland.

    • Text
    • [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987.
    • 1987
  • Studies on the flow induced by an oscillating airfoil in a uniform stream / door Zeguang Wang.

    • Text
    • Delft, Netherlands : Delft University Press, 1994.
    • 1994
    • 1 Item
    FormatCall NumberItem Location
    Text TL574.A4 W363 1994Off-site
  • A comparison of methods used in lifting surface theory : supplement to the Manual on aeroelasticity part VI / by D.L. Woodcock. --

    • Text
    • Neuilly-sur-Seine, France : AGARD, 1971.
    • 1971
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-583-71Off-site
  • Investigation of unsteady airloads on wings with oscillating control for active control purposes / by W. Geissler.

    • Text
    • Neuilly sur Seine, France : North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1981.
    • 1981
    • 1 Item
    FormatCall NumberItem Location
    Text AGARD-R-699Off-site
  • Studies on the flow induced by an oscillating airfoil in a uniform stream / door Zeguang Wang.

    • Text
    • Delft : Delft University Press, 1994.
    • 1994
    • 1 Item
    FormatCall NumberItem Location
    Text TL574.A4 W363 1994Off-site

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