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  1. 1
    Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61 /

    Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61 / by Brewer, Jack D.

    Published 1951
    Government Document Book
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  2. 2
    Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow /

    Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow / by Watkins, Charles E.

    Published 1950
    Government Document Book
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  3. 3
    A plan-form parameter for correlating certain aerodynamic characteristics of swept wings /

    A plan-form parameter for correlating certain aerodynamic characteristics of swept wings / by Diederich, Franklin W.

    Published 1951
    Government Document Book
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  4. 4
    Effect of aspect ratio on the low-speed lateral control characteristics of unswept untapered low-aspect-ratio wings /

    Effect of aspect ratio on the low-speed lateral control characteristics of unswept untapered low-aspect-ratio wings / by Naeseth, Rodger L.

    Published 1951
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  5. 5
    Effect of aspect ratio and sweepback on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with retractable ailerons /

    Effect of aspect ratio and sweepback on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with retractable ailerons / by Fischel, Jack

    Published 1951
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  6. 6
    A method for the rapid evaluation of Glauert's expressions for the angle of zero lift and the moment at zero lift /

    A method for the rapid evaluation of Glauert's expressions for the angle of zero lift and the moment at zero lift / by Pankhurst, R. C.

    Published 1944
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  7. 7
    Theoretical spanwise lift distributions of low-aspect-ratio wings at speeds below and above the speed of sound /

    Theoretical spanwise lift distributions of low-aspect-ratio wings at speeds below and above the speed of sound / by Diederich, Franklin W.

    Published 1949
    Government Document Book
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  8. 8
    Spanwise loading for wings and control surfaces of low aspect ratio /

    Spanwise loading for wings and control surfaces of low aspect ratio / by DeYoung, John

    Published 1950
    Government Document Book
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  9. 9
    The effects of sideslip, aspect ratio, and mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow /

    The effects of sideslip, aspect ratio, and mach number on the lift and pitching moment of triangular, trapezoidal, and related plan forms in supersonic flow / by Jones, A. L. (Arthur Leslie)

    Published 1949
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  10. 10
    Lift, pitching moment, and span load characteristics of wings at low speed as affected by variations of sweep and aspect ratio /

    Lift, pitching moment, and span load characteristics of wings at low speed as affected by variations of sweep and aspect ratio / by Hopkins, Edward J.

    Published 1951
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  11. 11
    Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45° sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord plain ailerons /

    Wind-tunnel investigation at low speed of lateral control characteristics of an untapered 45° sweptback semispan wing of aspect ratio 1.59 equipped with various 25-percent-chord pl... by Johnson, Harold S.

    Published 1951
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  12. 12
    Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds /

    Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds / by Turner, Thomas R.

    Published 1955
    Government Document Book
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  13. 13
    Correction of additional span loadings computed by the Weissinger seven-point method for moderately tapered wings of high aspect ratio /

    Correction of additional span loadings computed by the Weissinger seven-point method for moderately tapered wings of high aspect ratio / by DeYoung, John

    Published 1955
    Government Document Book
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  14. 14
    The transonic characteristics of 22 rectangular, symmetrical wing models of varying aspect ratio and thickness /

    The transonic characteristics of 22 rectangular, symmetrical wing models of varying aspect ratio and thickness / by Nelson, Warren H.

    Published 1955
    Government Document Book
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  15. 15
    Static longitudinal and lateral stability characteristics at low speed of unswept-midwing models having wings with an aspect ratio of 2, 4, or 6 /

    Static longitudinal and lateral stability characteristics at low speed of unswept-midwing models having wings with an aspect ratio of 2, 4, or 6 / by Wolhart, Walter D.

    Published 1956
    Government Document Book
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  16. 16
    Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6 /

    Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing mod... by Jaquet, Byron M.

    Published 1955
    Government Document Book
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  17. 17
    Summary of results obtained by transonic-bump method on effects of plan form and thickness on lift and drag characteristics of wings at transonic speeds /

    Summary of results obtained by transonic-bump method on effects of plan form and thickness on lift and drag characteristics of wings at transonic speeds / by Polhamus, Edward C. (Edward Charles), 1923-2001

    Published 1955
    Government Document Book
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  18. 18
    The transonic characteristics of 36 symmetrical wings of varying taper, aspect ratio, and thickness as determined by the transonic-bump technique /

    The transonic characteristics of 36 symmetrical wings of varying taper, aspect ratio, and thickness as determined by the transonic-bump technique / by Nelson, Warren H.

    Published 1955
    Government Document Book
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  19. 19
    Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings /

    Measurements of the effect of trailing-edge thickness on the zero-lift drag of thin low-aspect-ratio wings / by Morrow, John D.

    Published 1955
    Government Document Book
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  20. 20
    Drag interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02 /

    Drag interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02 / by Katzen, Elliott D.

    Published 1956
    Government Document Book
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