Showing 1 - 15 results of 15 for search 'Pendergraft, Odis C.', query time: 0.05s Refine Results
  1. 1
    Fuselage and nozzle pressure distributions of a 1/12-scale f-15 propulsion model at transonic speeds effect of fuselage modifications and nozzle variables /

    Fuselage and nozzle pressure distributions of a 1/12-scale f-15 propulsion model at transonic speeds effect of fuselage modifications and nozzle variables / by Pendergraft, Odis C.

    Published 1984
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  2. 2
    Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds /

    Fuselage and nozzle pressure distributions on a 1/12-scale F-15 propulsion model at transonic speeds / by Pendergraft, Odis C.

    Published 1979
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  3. 3
    A user's guide to the Langley 16- by 24-inch water tunnel

    A user's guide to the Langley 16- by 24-inch water tunnel by Pendergraft, Odis C.

    Published 1992
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  4. 4
    Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers /

    Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers / by Pendergraft, Odis C.

    Published 1982
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  5. 5
    Transonic aerodynamic characteristics of powered models of several Apollo launch-escape vehicle configurations /

    Transonic aerodynamic characteristics of powered models of several Apollo launch-escape vehicle configurations / by Berrier, Bobby L., Pendergraft, Odis C.

    Published 1968
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  6. 6
    Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /

    Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport / by Lamb, Milton, Carlson, John R., Pendergraft, Odis C.

    Published 1987
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  7. 7
    Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

    Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes by Foley, Robert J.

    Published 1991
    Other Authors: “…Pendergraft, Odis C.…”
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  8. 8
    Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

    Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds by Nugent, Jack

    Published 1987
    Other Authors: “…Pendergraft, Odis C.…”
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  9. 9
    An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds

    An experimental investigation of an advanced turboprop installation on a swept wing at subsonic and transonic speeds by Carlson, John R.

    Published 1987
    Other Authors: “…Pendergraft, Odis C.…”
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  10. 10
    A water tunnel study of gurney flaps

    A water tunnel study of gurney flaps by Neuhart, Dan H. (Dan Howard), 1952-

    Published 1988
    Other Authors: “…Pendergraft, Odis C.…”
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  11. 11
    Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model

    Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model

    Published 1992
    Other Authors: “…Pendergraft, Odis C.…”
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  12. 12
    Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds /

    Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds / by Bare, E. Ann

    Published 1983
    Other Authors: “…Pendergraft, Odis C.…”
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  13. 13
    Comparison of experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzles

    Comparison of experimental surface pressure with theoretical predictions on twin two-dimensional convergent-divergent nozzles by Carlson, John R.

    Published 1986
    Other Authors: “…Pendergraft, Odis C.…”
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  14. 14
    Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport

    Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport by Lamb, Milton

    Published 1987
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  15. 15
    Effect of pylon cross-sectional geometries on propulsion integration for a low-wing transport

    Effect of pylon cross-sectional geometries on propulsion integration for a low-wing transport by Ingraldi, Anthony M.

    Published 1993
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