Showing 1 - 20 results of 23 for search 'Re, Richard J.', query time: 0.06s Refine Results
  1. 1
    Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters /

    Static internal performance of single-expansion-ramp nozzles with various combinations of internal geometric parameters / by Re, Richard J.

    Published 1984
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  2. 2
    Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20 /

    Longitudinal aerodynamic characteristics of a fighter model with a close-coupled canard at Mach numbers from 0.40 to 1.20 / by Re, Richard J.

    Published 1978
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  3. 3
    Wind tunnel investigation of three axisymmetric cowls of different lengths at Mach numbers from 0.60 to 0.92

    Wind tunnel investigation of three axisymmetric cowls of different lengths at Mach numbers from 0.60 to 0.92 by Re, Richard J.

    Published 1993
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  4. 4
    Effect of varying internal geometry on the static performance of rectangular thrust-reverser ports

    Effect of varying internal geometry on the static performance of rectangular thrust-reverser ports by Re, Richard J.

    Published 1987
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  5. 5
    An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90 /

    An investigation of a close-coupled canard as a direct side-force generator on a fighter model at Mach numbers from 0.40 to 0.90 / by Re, Richard J.

    Published 1977
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  6. 6
    Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing /

    Static internal performance of single expansion-ramp nozzles with thrust vectoring and reversing / by Re, Richard J.

    Published 1982
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  7. 7
    Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration /

    Effect of several airframe/nozzle modifications on the drag of a variable-sweep bomber configuration / by Re, Richard J.

    Published 1979
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  8. 8
    An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 /

    An investigation of several NACA 1-series inlets at Mach numbers from 0.4 to 1.29 for mass-flow ratios near 1.0 / by Re, Richard J.

    Published 1976
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  9. 9
    Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles /

    Static internal performance including thrust vectoring and reversing of tow-dimensional convergent-divergent nozzles / by Re, Richard J.

    Published 1984
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  10. 10
    A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92

    A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 by Re, Richard J.

    Published 1996
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  11. 11
    An investigation of several NACA 1-series axisymmetric inlets at Mach numbers from 0.4 to 1.29 /

    An investigation of several NACA 1-series axisymmetric inlets at Mach numbers from 0.4 to 1.29 / by Re, Richard J.

    Published 1974
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  12. 12
    Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel

    Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel by Re, Richard J.

    Published 1998
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  13. 13
    Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft

    Static internal performance of ventral and rear nozzle concepts for short-takeoff and vertical-landing aircraft by Re, Richard J.

    Published 1991
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  14. 14
    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft / by Berrier, Bobby L., Re, Richard J.

    Published 1980
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  15. 15
    Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel /

    Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel / by Re, Richard J., Capone, Francis J.

    Published 1998
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  16. 16
    Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap /

    Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / by Re, Richard J., Leavitt, Laurence D.

    Published 1986
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  17. 17
    A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 /

    A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 / by Re, Richard J., Abeyounis, William Kelly

    Published 1996
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  18. 18
    Internal performance of a nonaxisymmetric nozzle with a rotating upper flap and a center-pivoted lower flap

    Internal performance of a nonaxisymmetric nozzle with a rotating upper flap and a center-pivoted lower flap by Wing, David J.

    Published 1993
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  19. 19
    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft

    Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft by Berrier, Bobby L.

    Published 1980
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  20. 20
    Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts /

    Effect of several geometric parameters on the static internal performance of three nonaxisymmetric nozzle concepts / by Berrier, Bobby L.

    Published 1979
    Other Authors: “…Re, Richard J.…”
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