Showing 1 - 19 results of 19 for search 'Beckwith, Ivan E.', query time: 0.09s Refine Results
  1. 1
    Heat transfer and skin friction by an integral method in the compressible laminar boundary layer with a streamwise pressure gradient /

    Heat transfer and skin friction by an integral method in the compressible laminar boundary layer with a streamwise pressure gradient / by Beckwith, Ivan E.

    Published 1953
    Government Document Book
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  2. 2
    Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15 /

    Heat transfer and recovery temperatures on a sphere with laminar, transitional, and turbulent boundary layers at Mach numbers of 2.00 and 4.15 / by Beckwith, Ivan E.

    Published 1957
    Government Document Book
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  3. 3
    Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling /

    Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling / by Beckwith, Ivan E.

    Published 1958
    Government Document Book
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  4. 4
    The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section /

    The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / by Beckwith, Ivan E.

    Published 1952
    Government Document Book
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  5. 5
    An accurate and rapid method for the design of supersonic nozzles /

    An accurate and rapid method for the design of supersonic nozzles / by Beckwith, Ivan E.

    Published 1955
    Government Document Book
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  6. 6
    Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling /

    Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling / by Beckwith, Ivan E.

    Published 1959
    Government Document Book
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  7. 7
    Similarity solutions for small cross flows in laminar compressible boundary layers /

    Similarity solutions for small cross flows in laminar compressible boundary layers / by Beckwith, Ivan E.

    Published 1961
    Government Document Book
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  8. 8
    Local heat transfer and recovery temperatures on a yawed cylinder at a mach number of 4.15 and high Reynolds numbers /

    Local heat transfer and recovery temperatures on a yawed cylinder at a mach number of 4.15 and high Reynolds numbers / by Beckwith, Ivan E.

    Published 1961
    Government Document Book
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  9. 9
    Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles /

    Görtler vortices and transition in wall boundary layers of two Mach 5 nozzles / by Beckwith, Ivan E.

    Published 1981
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  10. 10
    Detailed description and results of a method for computing mean and fluctuating quantities in turbulent boundary layers /

    Detailed description and results of a method for computing mean and fluctuating quantities in turbulent boundary layers / by Beckwith, Ivan E., Bushnell, Dennis M.

    Published 1968
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  11. 11
    The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section /

    The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / by Beckwith, Ivan E., Ridyard, Herbert W., Cromer, Nancy

    Published 1952
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  12. 12
    An accurate and rapid method for the design of supersonic nozzles /

    An accurate and rapid method for the design of supersonic nozzles / by Beckwith, Ivan E., Moore, J. A. (John Arnold)

    Published 1955
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  13. 13
    Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number /

    Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number / by Reshotko, Eli

    Published 1957
    Other Authors: “…Beckwith, Ivan E.…”
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  14. 14
    Free-stream noise and transition measurements on a cone in a Mach 3.5 pilot low-disturbance tunnel /

    Free-stream noise and transition measurements on a cone in a Mach 3.5 pilot low-disturbance tunnel /

    Published 1983
    Other Authors: “…Beckwith, Ivan E.…”
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  15. 15
    Investigation of the flow through a single-stage two-dimensional nozzle in the Langley 11-inch hypersonic tunnel /

    Investigation of the flow through a single-stage two-dimensional nozzle in the Langley 11-inch hypersonic tunnel / by McLellan, Charles H.

    Published 1950
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  16. 16
    Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel

    Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel by Creel, Theodore R.

    Published 1985
    Other Authors: “…Beckwith, Ivan E.…”
    Government Document Microfilm Book
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  17. 17
    Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5 /

    Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at mach 5 / by Creel, Theodore R.

    Published 1981
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  18. 18
    Correlations of supersonic boundary-layer transition on cones including effects of large axial variations in wind-tunnel noise /

    Correlations of supersonic boundary-layer transition on cones including effects of large axial variations in wind-tunnel noise / by Chen, Fang-Jenq

    Published 1984
    Other Authors: “…Beckwith, Ivan E.…”
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  19. 19
    Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield /

    Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield / by Creel, Theodore R.

    Published 1980
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