1–15 von 15 Ergebnissen
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    An algebraic model for dissipation in supersonic boundary layers

    HE, J. / KAZAKIA, J. / RUBAN, A. et al. | AIAA | 1992

    Application of an adaptive grid scheme for NPARC

    Mo, J / He, Z / Jin, K et al. | AIAA | 1995

    Departure from ideal performance in the linear induction launcher (LIL)

    LU, X. / LEVI, E. / ZABAR, Z. et al. | AIAA | 1992

    Design of space structure control systems using on-off thrusters

    VANDER VELDE / W. E. / HE, J. | AIAA | 1983

    Embedded function methods for supersonic turbulent boundary layers

    HE, J. / KAZAKIA, J. / WALKER, J. | AIAA | 1990

    Finite state induced flow models. II - Three-dimensional rotor disk

    Peters, David A. / He, Cheng J. | AIAA | 1995

    Numerical modeling of aerospike nozzle characteristics

    Zhao, Qingwei / Mo, J. / Chow, Alan et al. | AIAA | 2000

    Protein crystal growth aboard the U.S. space shuttle flights STS-31 and STS-32

    DeLucas, Lawrence J. / Smith, Craig D. / Carter, Daniel C. et al. | Elsevier | 1991

    Reply by the Authors to I. U. Ojalvo

    J. He / D. J. Ewinst | AIAA | 1992

    Test results of a high speed rotating heat pipe

    Ponnappan, R. / He, Q. / Leland, J. | AIAA | 1997

    Test Results of Water and Methanol High-Speed Rotating Heat Pipes

    R. Ponnappan / Q. He / J. E. Leland | AIAA | 1998

    Tether damping in space

    HE, XIAOHUA / POWELL, J. DAVID | AIAA | 1990