Showing 1 - 18 results of 18 for search '"Technical notes (United States. National Advisory Committee for Aeronautics) ;"', query time: 0.35s Refine Results
  1. 1
    Theoretical lift and damping in roll of thin sweptback tapered wings with raked-in and cross-stream wing tips at supersonic speeds /
    by Margolis, Kenneth
    Published 1950
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  2. 2
    Supersonic wave drag of sweptback tapered wings at zero lift /
    by Margolis, Kenneth
    Published 1947
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  3. 3
    Theoretical stability derivatives of thin sweptback wings tapered to a point with sweptback or sweptforward trailing edges for a limited range of supersonic speeds /
    by Malvestuto, Frank S
    Published 1949
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  4. 4
    Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds. : Subsonic leading edges and trailing edges /
    by Malvestuto, Frank S
    Published 1949
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  5. 5
    Lift and pitching moment at supersonic speeds due to constant vertical acceleration for thin sweptback tapered wings with streamwise tips. : Supersonic leading and trailing edges /
    by Cole, Isabella J
    Published 1954
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  6. 6
    Some remarks on an approximate method of estimating the wave drag due to thickness at supersonic speeds of three-dimensional wings with arbitrary profile /
    by Margolis, Kenneth
    Published 1952
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  7. 7
    Calculation of lift and pitching moments due to angle of attack and steady pitching velocity at supersonic speeds for thin sweptback tapered wings with streamwise tips and supersonic leading and trailing edges /
    by Martin, John C
    Published 1952
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  8. 8
    Theoretical calculations of the pressures, forces, and moments due to various lateral motions acting on thin isolated vertical tails with supersonic leading and trailing edges /
    by Margolis, Kenneth
    Published 1955
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  9. 9
    Theoretical calculations of the effects of finite sideslip at supersonic speeds on the span loading and rolling moment for families of thin sweptback tapered wings at an angle of attack /
    by Callaghan, Edmund E
    Published 1953
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  10. 10
    Theoretical calculation of the pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tipes parallel to the axis of wing symmetry /
    by Margolis, Kenneth
    Published 1953
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  11. 11
    Theoretical calculations of supersonic wave drag at zero lift for a particular store arrangement /
    by Margolis, Kenneth
    Published 1957
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  12. 12
    Effect of chordwise location of maximum thickness on the supersonic wave drag of sweptback wings /
    by Margolis, Kenneth
    Published 1948
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  13. 13
    Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips. : Subsonic leading edges and supersonic trailing edges /
    by Hannah, Margery E
    Published 1952
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  14. 14
    Flow over a slender body of revolution at supersonic velocities /
    by Jones, Robert T
    Published 1946
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  15. 15
    Supersonic wave drag of nonlifting sweptback tapered wings with Mach lines behind the line of maximum thickness /
    by Margolis, Kenneth
    Published 1948
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    Government Document Book
  16. 16
    Effect of thickness on the lateral force and yawing moment of a sideslipping delta wing at supersonic speeds /
    by Margolis, Kenneth
    Published 1949
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  17. 17
    Span load distributions resulting from constant vertical acceleration for thin sweptback tapered wings with streamwise tips. : Supersonic leading and trailing edges /
    by Cole, Isabella J
    Published 1954
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  18. 18
    Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips. : Subsonic leading edges /
    by Margolis, Kenneth
    Published 1950
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

    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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