1–20 von 34 Ergebnissen
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    Transient simulation of projectile fin heating/melt for hypersonic flyout

    York, B. / Kenzakowski, D. / Hosangadi, A. et al. | AIAA | 1997

    The F-111D computer complex

    DAGGETT, D. / LEE, R. | AIAA | 1968

    Tangential mass addition for shock/boundary-layer interaction control in scramjet inlets

    WHITE, M. E. / LEE, R. E. / THOMPSON, M. W. et al. | AIAA | 1991

    Scale model acoustic testing of counterrotating fans

    JANARDAN, B. / CHUANG, S. / HO, P. et al. | AIAA | 1988

    Recent work on an RF ion thruster

    LEE, R. / NAKANISHI, S. | AIAA | 1981

    Recent advances in jet/plume flowfield simulation

    Dash, S / Sinha, N / Kenzakowski, D et al. | AIAA | 1995

    Radiative cooling of a uniform gas flow.

    LEE, R. H. C. | AIAA | 1966

    On a supersonically charged shock tube

    Lee, R. / Fricker, D. | AIAA | 1996

    Nonorthogonal coordinates

    LEE, R. C. K. | AIAA | 1971

    Noise and emission outlook for military engines

    BAHR, D. / LEE, R. / TAYLOR, R. et al. | AIAA | 1973

    Nearly self-similar unsteady motion

    LEE, R. S. | AIAA | 1965

    Material Characterization of Shuttle Thermal Protection System for Impact Analyses

    W.-Y. Lu / B. Antoun / J. Korellis et al. | AIAA | 2005

    Hybrid, viscous, unstructured mesh solver for propulsive applications

    Hosangadi, A. / Lee, R. / Cavallo, P. et al. | AIAA | 1998