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  1. 1
    Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow /

    Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow / by Watkins, Charles E.

    Published 1951
    Government Document Book
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  2. 2
    Lift and moment on oscillating triangular and related wings with supersonic edges /

    Lift and moment on oscillating triangular and related wings with supersonic edges / by Nelson, Herbert C.

    Published 1951
    Government Document Book
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  3. 3
    Three-dimensional unsteady lift problems in high-speed flight : the triangular wing /

    Three-dimensional unsteady lift problems in high-speed flight : the triangular wing / by Lomax, Harvard

    Published 1951
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  4. 4
    Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges

    Experimental surface pressure data obtained on 65̊ delta wing across Reynolds number and Mach number ranges by Chu, Julio

    Published 1996
    Government Document Microfilm Book
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  5. 5
    Preliminary investigation at supersonic speeds of triangular and sweptback wings /

    Preliminary investigation at supersonic speeds of triangular and sweptback wings / by Ellis, Macon C.

    Published 1949
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  6. 6
    Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model /

    Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model / by Lovell, Powell M.

    Published 1957
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  7. 7
    Damping in roll of cruciform and some related delta wings at supersonic speeds /

    Damping in roll of cruciform and some related delta wings at supersonic speeds / by Ribner, H. S. (Herbert S.), 1913-

    Published 1951
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  8. 8
    Flow studies on flat-plate delta wings at supersonic speed /

    Flow studies on flat-plate delta wings at supersonic speed / by Michael, William H.

    Published 1955
    Government Document Book
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  9. 9
    Comparison between experimental and predicted downwash at a Mach number of 0.25 behind a wing-body combination having a triangular wing of aspect ratio 2.0 /

    Comparison between experimental and predicted downwash at a Mach number of 0.25 behind a wing-body combination having a triangular wing of aspect ratio 2.0 / by Sorensen, Norman E., 1930-

    Published 1956
    Government Document Book
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  10. 10
    On slender delta wings with leading-edge separation /

    On slender delta wings with leading-edge separation / by Brown, Clinton E.

    Published 1955
    Government Document Book
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  11. 11
    Experimental steady-state yawing deriviatives of a 60 degree delta-wing model as affected by changes in vertical position of the wing and in ratio of fuselage diameter to wing span /

    Experimental steady-state yawing deriviatives of a 60 degree delta-wing model as affected by changes in vertical position of the wing and in ratio of fuselage diameter to wing span... by Jaquet, Byron M.

    Published 1956
    Government Document Book
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  12. 12
    Analysis of multicell delta wings on Cal-Tech analog computer /

    Analysis of multicell delta wings on Cal-Tech analog computer / by MacNeal, R. (Richard)

    Published 1953
    Government Document Book
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  13. 13
    Velocity potential and air forces associated with a triangular wing in supersonic flow, with subsonic leading edges, and deforming harmonically according to a general quadratic equation /

    Velocity potential and air forces associated with a triangular wing in supersonic flow, with subsonic leading edges, and deforming harmonically according to a general quadratic equ... by Watkins, Charles E.

    Published 1953
    Government Document Book
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  14. 14
    Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bump method /

    Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bump method / by Emerson, Horace F.

    Published 1956
    Government Document Book
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  15. 15
    Deflection of delta wings having a carry-through-bay chord smaller than the wing root chord /

    Deflection of delta wings having a carry-through-bay chord smaller than the wing root chord / by Peters, Roger W.

    Published 1953
    Government Document Book
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  16. 16
    A new shadowgraph technique for the observation of conical flow phenomena in supersonic flow and preliminary results obtained for a triangular wing /

    A new shadowgraph technique for the observation of conical flow phenomena in supersonic flow and preliminary results obtained for a triangular wing / by Love, Eugene S.

    Published 1953
    Government Document Book
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  17. 17
    Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing /

    Low-speed wind-tunnel investigation of a triangular sweptback air inlet in the root of a 45 degree sweptback wing / by Keith, Arvid L.

    Published 1955
    Government Document Book
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  18. 18
    The zero-lift drag of a 60 degree delta-wing-body combination (AGARD Model 2) obtained from free-flight tests between Mach numbers of 0.8 and 1.7 /

    The zero-lift drag of a 60 degree delta-wing-body combination (AGARD Model 2) obtained from free-flight tests between Mach numbers of 0.8 and 1.7 / by Piland, Robert O.

    Published 1954
    Government Document Book
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  19. 19
    Lift and moment on thin arrowhead wings with supersonic edges oscillating in symmetric flapping and roll and application to the flutter of an all-movable control surface /

    Lift and moment on thin arrowhead wings with supersonic edges oscillating in symmetric flapping and roll and application to the flutter of an all-movable control surface / by Cunningham, Herbert J.

    Published 1958
    Government Document Book
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  20. 20
    Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings at supersonic speeds /

    Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings at supersonic speeds / by Bobbitt, Percy J.

    Published 1956
    Government Document Book
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