1–20 of 432 hits
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    Measurements of test time in the galcit 17-inch shock tube

    ROSHKO, A. / SMITH, J. A. | AIAA | 1964

    Internal and external aerodynamics of the c-141a nacelle

    SAYLOR, J. / SMITH, JR., R. | AIAA | 1965

    A variational method for optimal staging.

    DICKERSON, W. D. | AIAA | 1965

    Protection of graphite from oxidation at 2100 deg C.

    CRISCIONE, J. M. / SMITH, A. W. | AIAA | 1966

    Effect of injection distribution on combustion stability.

    MCBRIDE, J. M. / REARDON, F. H. / SMITH, A. J. | AIAA | 1966

    Some comparisons of turboramjet-powered hypersonic aircraft for cruise and boost missions.

    GREGORY, T. J. / PETERSEN, R. H. / SMITH, C. L. | AIAA | 1966

    On predicting thermal conductivity of a binary mixture of solids.

    FOSTER, J. M. / SMITH, C. B. / VACHON, R. I. | AIAA | 1966

    Techniques used to conduct external burning experiments in the shocktunnel

    COPPER, J. / GRIFFITH, W. / HAMEETMAN, F. et al. | AIAA | 1966

    Application of the Mira 150A variable-thrust engine to manned lunar flying systems.

    BOYD, B. R. / JOHNSON, R. J. / SMITH, T. H. | AIAA | 1968