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    Research on radiational active thermal control technology for spacecraft

    ZHANG, Z. / GUO, S. / SUN, Y. et al. | AIAA | 1980

    The experimental investigation of combustion efficiency of air-augmented rockets

    ZHANG, Z. / TAO, J. / FENG, W. | AIAA | 1985

    The measurement of exhaust velocity of pulsed plasma thruster

    PANG, H.-X. / ZHANG, Z.-Y. | AIAA | 1985

    Structure of nonevaporating sprays. II - Drop and turbulence properties

    SOLOMON, A. S. P. / SHUEN, J.-S. / ZHANG, Q.-Z. et al. | AIAA | 1985

    Experimental investigation of combustion efficiency of air-augmentedrockets

    ZHANG, Z. / TAO, J. / FANG, W. | AIAA | 1986

    Design of a supercritical airfoil

    ZHANG, Z. Y. / YANG, X. T. / LASCHKA, B. | AIAA | 1988

    Fundamental turbulence measurements by relief flow tagging

    MILES, RICHARD / LEMPERT, WALTER / ZHANG, BOYING et al. | AIAA | 1992

    Thermally developing convection from Newtonian flow in rectangular ducts with uniform heating

    CHUNG, B. T. F. / ZHANG, Z. J. / LI, G. et al. | AIAA | 1993

    Study of High Thrust Ratio Approaches for Single-Chamber Dual-Thrust Solid Rocket Motors

    HU, K. / ZHANG, Y. / CAI, X. et al. | AIAA | 1994

    Augmented heat transfer in triangular ducts with full and partial ribbed walls

    Zhang, Y. M. / Gu, W. Z. / Han, J. C. | AIAA | 1994

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