1–20 von 33 Ergebnissen
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    Material Characterization of Shuttle Thermal Protection System for Impact Analyses

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

    Application of unstructured-grid methodology to scramjet combustor flowfields

    Lee, R. / Hosangadi, A. / Cavallo, P. et al. | AIAA | 1999

    Aero-propulsive jet interaction simulations using hybrid unstructured meshes

    Hosangadi, A. / Cavallo, P. / Arunajatesan, S. et al. | AIAA | 1999

    Antioptimization for Comparison of Alternative Structural Models and Damage Detection

    S. Gangadharan / E. Nikolaidis / K. Lee et al. | AIAA | 1999

    Hybrid, viscous, unstructured mesh solver for propulsive applications

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

    Transient simulation of projectile fin heating/melt for hypersonic flyout

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

    On a supersonically charged shock tube

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

    Recent advances in jet/plume flowfield simulation

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

    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

    Advanced mass memories

    SCHWEE, L. / ANDERSON, W. / LIU, Y. et al. | AIAA | 1977

    Buoyancy effects on a turbulent shear flow

    LEE, R. H. C. / CHUNG, P. M. | AIAA | 1975

    Noise and emission outlook for military engines

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