1–11 von 11 Ergebnissen
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    Subsonic pitch-up alleviation on a 74 deg delta wing

    Rao, D. M. / Johnson, T. D., Jr. | NTRS | 1981

    Anti-swirl vanes for vortex upset alleviation

    Wentz, Jr., W. / Nagati, M. / Christmore, D. | AIAA | 1999

    Lee-side vortices on delta wings at hypersonic speeds.

    Rao, D. M. / Whitehead, A. H., Jr. | NTRS | 1972

    Transformation of Hypersonic Turbulent Boundary Layers to Incompressible Form

    Cary, Aubrey M., Jr. / Watson, Ralph D. | NTRS | 1967

    Interactive systems design and synthesis of future spacecraft concepts

    Wright, R. L. / Deryder, D. D. / Ferebee, M. J., Jr. | NTRS | 1984

    Mixing length in low Reynolds number compressible turbulent boundary layers

    Bushnell, D. M. / Cary, A. M., Jr. / Holley, B. B. | NTRS | 1975

    Development of a Two-Level Output Vehicle Safety Device Initiated by the Driver’s Eye Movement Patterns

    Tolentino, Efren Victor Jr. N. / Retumban, Joseph D. / Dimalibot, Dann Adrian A. et al. | Springer Verlag | 2021

    Aeroassist flight experiment heating-rate sensitivity study

    ROCHELLE, W. C. / TING, P. C. / BOUSLOG, S. A. et al. | AIAA | 1991