1–20 of 23 hits
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    Jupiter entry probe afterbody convective heating

    BALAKRISHNAN, A. / CHU, E. | AIAA | 1979

    Radiative viscous-shock-layer analysis of Fire, Apollo, and PAET flight data

    BALAKRISHNAN, A. / PARK, C. / GREEN, M. | AIAA | 1985

    Real-gas flowfields about three-dimensional configurations

    BALAKRISHNAN, A. / LOMBARD, C. K. / DAVY, W.C. | AIAA | 1985

    Configuration impact on heat shield requirements for Jupiter entry

    NICOLET, W. / BALAKRISHNAN, A. / MEZINES, S. | AIAA | 1976

    Real gas flow fields about three dimensional configurations

    BALAKRISHNAN, A. / LOMBARD, C. / DAVY, W.C. | AIAA | 1983

    Aerothermodynamic environment for a Titan probe with deployable decelerator

    GREEN, M. / SWENSON, B. / BALAKRISHNAN, A. | AIAA | 1985

    Simulating AOTV heating environment in an arc jet

    BALBONI, J. / WINOVICH, W. / BALAKRISHNAN, A. | AIAA | 1986