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person:(Jackson, C.)

    Penetration heights of liquid jets in high-speed crossflows

    Lin, K.-C. / Kennedy, P. / Jackson, T. | AIAA | 2002

    Structures of aerated-liquid jets in subsonic crossflows

    Lin, K.-C. / Kennedy, P. / Jackson, T. | AIAA | 2001

    An operational electrothermal propulsion system for spacecraft reaction control

    HAGELBERG, C. / JACKSON, F. / JORTNER, D. | AIAA | 1966

    Closed-loop simulation of inertial platform accelerometer inputs

    JACKSON, C. T. / SCHLOETZER, F. F. | AIAA | 1965

    Breakup of Aerated-Liquid Jets in Supersonic Crossflows

    Sallam, K. / Aalburg, C. / Faeth, G. et al. | AIAA | 2004

    Spray structures of aerated liquid fuel jets in supersonic crossflows

    Lin, K.-C. / Kirkendall, K. / Kennedy, P. et al. | AIAA | 1999

    Supersonic combustion experiments with a cavity-based fuel injector

    Mathur, T. / Streby, G. / Gruber, M. et al. | AIAA | 1999

    The PIT Mark VI Pulsed Inductive Thruster

    Russell, Derrek / Dailey, C. / Goldstein, Wayne et al. | AIAA | 2004

    Ram-Air-Spoiler Roll Stabilization Device for Forward-Control Cruciform Missiles

    A.B. Blair Wallace C. Sawyer / Charlie M. Jackson | AIAA | 1979