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  1. 1
    Transient growth theory prediction of optimal placing of passive and active flow control devices for separation delay in LPT airfoils /
    by Tumin, Anatoli
    Published 2003

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    Government Document Book
  2. 2
    Robust airfoil optimization to achieve consistent drag reduction over a mach range /
    by Li, Wu, Li, Wu
    Published 2001

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    Government Document Book
  3. 3
    The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil : suction coefficient analysis /

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    Government Document Book
  4. 4
    On central-difference and upwind schemes /

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    Government Document Book
  5. 5
    Development and testing of airfoils for high-altitude aircraft final report /
    by Drela, Mark
    Published 1996

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    Government Document Book
  6. 6
    Numerical solutions of the complete Navier-Stokes equations progress report no. 27 for the period October 1, 1995 to September 30, 1996 /
    by Hassan, H. A
    Published 1996

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    Government Document Book
  7. 7
    Effect of a rotor wake on the local heat transfer on the forward half of a circular cylinder
    by Morehouse, Kim A
    Published 1986

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    Government Document Book
  8. 8
    In-flight measurements of wing ice shapes and wing section drag increases caused by natural icing conditions /
    Published 1986

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    Government Document Book
  9. 9
    Heat transfer in aeropropulsion systems
    by Simoneau, Robert J
    Published 1985

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  10. 10
    Convective heat transfer measurements from a NACA 0012 airfoil in flight and in the NASA Lewis icing research tunnel /

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    Government Document Book
  11. 11
    Trailing edge flow conditions as a factor in airfoil design /
    by Ormsbee, A. I
    Published 1984

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    Government Document Book
  12. 12
    Final report for the period January 1, 1974 through December 31, 1983 entitled : Numerical solution of the Navier-Stokes equations for arbitrary two-dimensional multi-element airfoils
    by Thompson, Joe F
    Published 1983

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  13. 13
    A cooperative program to stimulate student involvement through the MIT undergraduate research opportunity program final report /
    Published 1984

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  14. 14
    A Modified lifted line theory for wing-propeller interference progress report for the period June 1 to September 30, 1983 /
    by Prabhu, R. K
    Published 1983

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  15. 15
    A lifting surface theory in rotational flow
    by Shiau, Mawshyong Jack
    Published 1983

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  16. 16
    Control of flow separation and mixing by aerodynamic excitation /
    by Rice, Edward J, Rice, Edward J
    Published 1990

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  17. 17
    Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet /
    Published 2002

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    Government Document Book
  18. 18
    Semiempirical method for predicting vortex-induced rolling moments /
    by Allison, Dennis O
    Published 1985

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    Government Document Book
  19. 19
    Advanced turbine study final report /
    Published 1985

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Electronic Book
  20. 20
    Optimization of an advanced design three-element airfoil at high Reynolds numbers /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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