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  1. 1
    Laminar-boundary-layer heat-transfer characteristics of a body of revolution with a pressure gradient at supersonic speeds /

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

    Published 1950
    Government Document Book
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  2. 2
    Variation of boundary-layer transition with heat transfer on two bodies of revolution at a Mach number of 3.12 /

    Variation of boundary-layer transition with heat transfer on two bodies of revolution at a Mach number of 3.12 / by Jack, John R.

    Published 1955
    Government Document Book
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  3. 3
    Heat-transfer measurements on two bodies of revolution at a Mach number of 3.12 /

    Heat-transfer measurements on two bodies of revolution at a Mach number of 3.12 / by Jack, John R.

    Published 1956
    Government Document Book
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  4. 4
    An extension of the investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 /

    An extension of the investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 / by Czarnecki, K. R.

    Published 1954
    Government Document Book
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  5. 5
    Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 /

    Preliminary investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 / by Czarnecki, K. R.

    Published 1954
    Government Document Book
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  6. 6
    Theoretical and experimental investigation of aerodynamic-heating and isothermal heat-transfer parameters on a hemispherical nose with laminar boundary layer at supersonic Mach numbers /

    Theoretical and experimental investigation of aerodynamic-heating and isothermal heat-transfer parameters on a hemispherical nose with laminar boundary layer at supersonic Mach num... by Stine, Howard A.

    Published 1954
    Government Document Book
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  7. 7
    Effects of Mach number and wall-temperature ratio on turbulent heat transfer at Mach numbers from 3 to 5 /

    Effects of Mach number and wall-temperature ratio on turbulent heat transfer at Mach numbers from 3 to 5 / by Tendeland, Thorval

    Published 1958
    Government Document Book
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  8. 8
    Correlation of supersonic convection heat-transfer coefficients from measurements of the skin temperature of a parabolic body of revolution (NACA RM-10) /

    Correlation of supersonic convection heat-transfer coefficients from measurements of the skin temperature of a parabolic body of revolution (NACA RM-10) / by Chauvin, Leo T.

    Published 1956
    Government Document Book
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  9. 9
    A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61 /

    A note on the effect of heat transfer on peak pressure rise associated with separation of turbulent boundary layer on a body of revolution (NACA RM-10) at a Mach number of 1.61 / by Czarnecki, K. R.

    Published 1957
    Government Document Book
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  10. 10
    Preliminary heat-transfer studies on two bodies of revolution at angle of attack at a Mach number of 3.12 /

    Preliminary heat-transfer studies on two bodies of revolution at angle of attack at a Mach number of 3.12 / by Sands, Norman

    Published 1958
    Government Document Book
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  11. 11
    The Effects of aerodynamic heating and heat transfer on the surface temperature of a body of revolution in steady supersonic flight /

    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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  12. 12
    Investigation of heat transfer from a stationary and rotating ellipsoidal forebody of fineness ratio 3 /

    Investigation of heat transfer from a stationary and rotating ellipsoidal forebody of fineness ratio 3 / by Lewis, James P.

    Published 1956
    Government Document Book
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