51–60 of 197 hits
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    Pitch Axis Stabilization in Eccentric Orbits Using a Variable-Speed Rotor

    R. E. LOHFELD / D. K. ANAND AND J. M. WHISNANT | AIAA | 1974

    Performance of differenced range data types in Voyager navigation

    TAYLOR, T. H. / CAMPBELL, J. K. / JACOBSON, R. A. et al. | AIAA | 1984

    Performance of a Low Density Ablative Heat Shield Material

    Covington, M. A. / Balboni, J. A. / Chen, Y-K et al. | AIAA | 2004

    Performance degradation of a model helicopter rotor with a generic ice shape

    KORKAN, K. D. / CROSS, E. J. / MILLER, T. L. | AIAA | 1984

    Performance Cycle Analysis of Turbofan Engine with Interstage Turbine Burner

    K. H. Liew / E. Urip / S. L. Yang et al. | AIAA | 2006

    Passive control of flow separation over delta wings at high angle-of-attack

    Van Dyken, R. / Yu, K. / Gutmark, E. et al. | AIAA | 1996

    Parameter identification and modeling of longitudinal aerodynamics

    Aksteter, J. W. / Parks, E. K. / Bach, R. E. | AIAA | 1995

    Parallelization of direct simulation Monte Carlo method combined with monotonic Lagrangian grid

    Oh, C. K. / Sinkovits, R. S. / Cybyk, B. Z. et al. | AIAA | 1996

    Orbit determination using analytic partial derivatives of perturbed motion

    ARSENAULT, J. L. / FORD, K. C. / KOSKELA, P. E. | AIAA | 1970