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    Methods for the analysis of high-pressure, high-enthalpy constrictedarc heaters

    NICOLET, W. / SHEPARD, C. / CLARK, K. et al. | AIAA | 1975

    Configuration impact on heat shield requirements for Jupiter entry

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

    Jupiter entry probe afterbody convective heating

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

    Real gas flow fields about three dimensional configurations

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

    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

    Aerothermodynamic environment for a Titan probe with deployable decelerator

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

    Radiometer experiment for the aeroassist flight experiment

    DAVY, W. / PARK, C. / ARNOLD, J. et al. | AIAA | 1985

    Real-gas flowfields about three-dimensional configurations

    Balakrishnan, A. / Lombard, C. K. / Davy, W. C. | NTRS | 1985