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  1. 1
    Pressure measurements for Mach five flows over winged re-entry configurations with aerodynamic controls.

    Pressure measurements for Mach five flows over winged re-entry configurations with aerodynamic controls. by Kaufman, Louis G.

    Published 1964
    Government Document Book
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  2. 2
    Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds /

    Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds / by Jackson, Mary W., Czarnecki, K. R.

    Published 1960
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  3. 3
    Computation of asymmetric supersonic flows around cones at large incidence final report /

    Computation of asymmetric supersonic flows around cones at large incidence final report / by Degani, David

    Published 1987
    Government Document Microfilm Book
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  4. 4
    Viscous shock layer solutions for hypersonic sphere-cones / prepared by Department of Aerospace Engineering, University of Cincinnati; authors: B.N. Srivastava, M.J. Werle, and R.T. Davis.

    Viscous shock layer solutions for hypersonic sphere-cones / prepared by Department of Aerospace Engineering, University of Cincinnati; authors: B.N. Srivastava, M.J. Werle, and R.T... by Srivastava, B. N., Werle, M. J., Davis, R. T.

    Published 1977
    Government Document Book
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  5. 5
    Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes /

    Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes / by Bobbitt, Percy J.

    Published 2012
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  6. 6
    Blowing from a porous cone or wedge when the contact surface is straight.

    Blowing from a porous cone or wedge when the contact surface is straight.

    Published 1966
    Government Document Book
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  7. 7
    An integral method solution for massive blowing from slender bodies in laminar viscous hypersonic flow.

    An integral method solution for massive blowing from slender bodies in laminar viscous hypersonic flow.

    Published 1966
    Government Document Book
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  8. 8
    Effect of contact surface bluntness on massive blowing from a wedge in hypersonic flow.

    Effect of contact surface bluntness on massive blowing from a wedge in hypersonic flow.

    Published 1966
    Government Document Book
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  9. 9
    Correlation of transonic-cone Preston-tube data and skin friction final report (research grant number NAG 2-76) (Nov. 80 - May 84) /

    Correlation of transonic-cone Preston-tube data and skin friction final report (research grant number NAG 2-76) (Nov. 80 - May 84) / by Abu-Mostafa, A. (Ayman), 1953-

    Published 1984
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  10. 10
    DSMC calcuations for a 70⁰ blunted cone at 3.2km/s in nitrogen

    DSMC calcuations for a 70⁰ blunted cone at 3.2km/s in nitrogen by Moss, J. N.

    Published 1995
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  11. 11
    Analysis of flight data on boundary layer transition at high angles of attack /

    Analysis of flight data on boundary layer transition at high angles of attack / by Haigh, Wayne W.

    Published 1972
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  12. 12
    Analysis of flowfields over four-engine DC-X rockets

    Analysis of flowfields over four-engine DC-X rockets by Wang, Ten-See, 1950-

    Published 1996
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