1–20 of 23 hits
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    Applied resistojet technology

    PUGMIRE, T. / SHAW, R. | AIAA | 1970

    Ice shapes and the resulting drag increase for a NACA 0012 airfoil

    OLSEN, W. / SHAW, R. / NEWTON, J. | AIAA | 1984

    An analytical approach to airfoil icing

    BRAGG, M. / GREGOREK, G. / SHAW, R. | AIAA | 1981

    An experimental study of airfoil icing characteristics

    SHAW, R. / SOTOS, R. / SOLANO, F. | AIAA | 1982

    Minimizing boundary layer bleed for a mixed compression inlet

    WASSERBAUER, J. / SHAW, R. / NEUMANN, H. | AIAA | 1973

    VSTOL tilt nacelle aerodynamics and its relation to fan blade stresses

    SHAW, R. / WILLIAMS, R. / KONCSEK, J. | AIAA | 1978

    Performance degradation of propeller systems due to rime ice accretion

    KORKAN, K. / DADONE, L. / SHAW, R. | AIAA | 1982

    NASA Lewis Research Center's program on icing research

    REINMANN, J. / SHAW, R. / OLSEN, JR., W. | AIAA | 1983

    Performance degradation of helicopter rotor in forward flight due toice

    KORKAN, K. D. / DADONE, L. / SHAW, R. J. | AIAA | 1985

    Helicopter rotor performance degradation in natural icing encounter

    KORKAN, K. D. / DADONE, L. / SHAW, R. J. | AIAA | 1984

    Performance degradation of propeller systems due to rime ice accretion

    KORKAN, K. D. / DADONE, L. / SHAW, R. J. | AIAA | 1984

    ELECTROTHERMAL HYDRAZINE ENGINE PERFORMANCE

    PUGMIRE, T.K. / OCONNOR, T. / SHAW, R. et al. | AIAA | 1971