1–15 of 15 hits
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    Heat shielding for Venus entry probes

    PETERSON, D. / NICOLET, W. | AIAA | 1973

    Outer planet probe entry thermal protection. I Aerothermodynamic environment

    NICOLET, W. / VOJVODICH, N. / MORSE, H. | AIAA | 1974

    Configuration impact on heat shield requirements for Jupiter entry

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

    Viscous hypersonic flow over complex bodies at high angles of attack

    SRINIVASAN, G. / NICOLET, W. / SHANKS, S. | AIAA | 1984

    Heat-shield ablation at superorbital re-entry velocities

    BARTLETT, E. / HOWE, J. / NICOLET, W. | AIAA | 1970

    Methods for predicting radiation coupled flowfields about planetary entry probes

    NICOLET, W. / WATERLAND, L. / KENDALL, R. | AIAA | 1977

    Flowfield predictions about lifting entry vehicles

    NICOLET, W. / SHANKS, S. / SRINIVASAN, G. et al. | AIAA | 1982

    An investigation of hydrometeor shock layer interaction

    NICOLET, W. / WOOL, M. / LAUB, B. et al. | AIAA | 1976

    Flow field prediction and analysis, project fire final report

    Buckingham, A. C. / Hoshizaki, H. / Nicolet, W. E. et al. | NTRS | 1965

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

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