Search Results - Scherrer, R.

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  1. 1
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    Comparison of theoretical and experimental heat transfer on a cooled 20 degree cone with a laminar boundary layer at a Mach number of 2.02 / by Scherrer, R.

    Published 1950
    Government Document Book

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  2. 2
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    Preliminary investigation of a family of diffusers designed for near sonic inlet velocities / by Scherrer, R.

    Published 1956
    Government Document Book

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  3. 3
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    Boundary-layer transition on a cooled 20° cone at Mach numbers of 1.5 and 2.0 / by Scherrer, R.

    Published 1950
    Government Document Book

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  4. 4
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    An analytical investigation of a thermal-electric means of preventing ice formations on a propeller blade / by Scherrer, R.

    Published 1944
    Government Document Book

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  5. 5
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    An investigation of the characteristics of alcohol-distribution tubes used for ice protection on aircraft windshields / by Scherrer, R.

    Published 1944
    Government Document Book

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  6. 6
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    Tests of thermal-electric de-icing equipment for propellers / by Scherrer, R.

    Published 1944
    Government Document Book

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  7. 7
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    Flight tests of thermal ice-prevention equipment on a Lockheed 12A airplane / by Scherrer, R.

    Published 1943
    Government Document Book

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  8. 8
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    A flight investigation of fuselage static-pressure-vent airspeed installations / by Scherrer, R.

    Published 1943
    Government Document Book

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  9. 9
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    The Effects of aerodynamic heating and heat transfer on the surface temperature of a body of revolution in steady supersonic flight / by Scherrer, R.

    Published 1947
    Government Document Book

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  10. 10
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    Design and calibration of a total-temperature probe for use at supersonic speeds / by Goldstein, David L.

    Published 1949
    Other Authors: “…Scherrer, R.…”
    Government Document Book

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  11. 11
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    Experimental investigation of the turbulent-boundary-layer temperature-recovery factor on bodies of revolution at Mach numbers from 2.0 to 3.8 / by Stine, Howard A.

    Published 1952
    Other Authors: “…Scherrer, R.…”
    Government Document Book

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  12. 12
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    Laminar-boundary-layer heat-transfer characteristics of a body of revolution with a pressure gradient at supersonic speeds / by Wimbrow, William R.

    Published 1950
    Other Authors: “…Scherrer, R.…”
    Government Document Book

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  13. 13
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    The solar dynamics observatory

    Published 2012
    “…J. Schou, P.H. Scherrer, R.I. Bush, R. Wachter and S. Couvidat, et …”
    Full Text (via Springer)
    Electronic eBook

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  14. 14
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    Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058

    Published 1952
    Other Authors: “…Scherrer, R.…”
    Online Access
    Government Document Electronic eBook

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