Showing 141 - 160 results of 5,412 for search '"Technical notes (United States. National Advisory Committee for Aeronautics) ;"', query time: 5.89s Refine Results
  1. 141
    Effects of wing position and horizontal-tail position on the static stability characteristics of models with unswept and 45 degrees sweptback surfaces with some reference to mutual interference /
    by Goodman, Alex
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  2. 142
    An Experimental investigation of the NACA 63₁-012 airfoil section with leading-edge and midchord suction slots /
    by McCullough, George B
    Published 1950
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  3. 143
    Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes /
    by Riebe, John M
    Published 1952
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  4. 144
    Approximate methods for calculating the flow about nonlifting bodies of revolution at high high supersonic airspeeds /
    by Eggers, A. J
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  5. 145
    Time-dependent downwash at the tail and the pitching moment due to normal acceleration at supersonic speeds /
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  6. 146
    Lift and moment on oscillating triangular and related wings with supersonic edges /
    by Nelson, Herbert C
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  7. 147
    Wind-tunnel investigation of effects of various aerodynamic balance shapes and sweepback on control-surface characteristics of semispan tail surfaces with NACA 0009, 0015, 66-009, 66(215)-014, and circular-arc airfoil sections /
    by Harper, John J
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  8. 148
    Stability and control characteristics of a complete airplane model having a wing with quarter-chord line swept back 40 degrees, aspect ratio 2.50, and taper ratio 0.42 /
    by Schuldenfrei, Marvin
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  9. 149
    Hydrodynamic characteristics of a low-drag, planing-tail flying-boat hull /
    by Suydam, Henry B
    Published 1952
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  10. 150
    A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory /
    by Matthews, Clarence W
    Published 1953
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  11. 151
    An investigation of aircraft heaters
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  12. 152
    Examples of three representative of airfoil-section stall at low speed /
    by McCullough, George B
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  13. 153
    Wind-tunnel investigation and analysis of the effects of end plates on the aerodynamic characteristics of an unswept wing /
    by Riley, Donald R
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  14. 154
    Some measurements of the effect of gaseous imperfections on the critical pressure ratio in air and the speed of sound in nitrogen /
    by Donaldson, Coleman duP
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  15. 155
    Width of Debye-Scherrer lines for finite spectral width of primary beam /
    by Ekstein, Hans
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  16. 156
    Investigation at low speed of 45 degrees and 60 degrees sweptback, tapered, low-drag wings equipped with various types of full-span, trailing-edge flaps /
    by Harper, John J
    Published 1951
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  17. 157
    Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter /
    by Reeder, John P
    Published 1952
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  18. 158
    The effects of Reynolds number on the application of NACA 16-series airfoil characteristics to propeller design /
    by Cleary, Harold E
    Published 1952
    “...Technical note (United States. National Advisory Committee for Aeronautics) ;...”

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    Government Document Book
  19. 159
    Tables of wing-aileron coefficients of oscillating air forces for two-dimensional supersonic flow /
    by Huckel, Vera
    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
  20. 160
    Flight investigation of the effect of atmospheric turbulence on the climb performance of an airplane /
    by Press, Harry
    Published 1951
    “...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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