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    Variable cycle engines - The next step in propulsion evolution

    JOHNSON, J. | AIAA | 1976

    A pure fluid absolute pressure ratio sensor

    JOHNSON, J. | AIAA | 1966

    Update on development of the Space Shuttle main engine /as of 5 May 1977/

    JOHNSON, J. | AIAA | 1977

    Site bench maintenance test set

    JOHNSON, J. | AIAA | 1964

    Maximum errors from quantization in multirate digital control systems

    JOHNSON, J. C. | AIAA | 1970

    A hybrid structured/unstructured grid multi-block flow solver for distributed parallel processing

    Michal, T. / Johnson, J. | AIAA | 1997

    Space Shuttle main engine progress through the first flight

    JOHNSON, J. / COLBO, H. | AIAA | 1981

    Application of advanced technologies to improve C-141 cruise performance<149>wing modifications for drag reduction

    BLACKERBY, W. / JOHNSON, J. | AIAA | 1979

    Starting phenomena in a supersonic tube wind tunnel

    CAGLIOSTRO, D. / JOHNSON, J. A. | AIAA | 1971

    Update on the development of the Space Shuttle main engine /as of June 20, 1978/

    JOHNSON, J. / COLBO, H. | AIAA | 1978

    Tapered roller bearing adjustment lessons learned

    EMMERLING, W. / JOHNSON, J. | AIAA | 1992

    Full power level development of the Space Shuttle main engine

    JOHNSON, J. / COLBO, H. | AIAA | 1982

    Intelsat V spacecraft design summary

    RUSCH, R. / JOHNSON, J. / BAER, W. | AIAA | 1978

    On the development and pre-flight testing of the affordable guided airdrop system for G-12 cargo parachute

    Johnson, J. / Yakimenko, O. / Kaminer, L. et al. | AIAA | 2001

    Calculation of vortex flowfields around forebodies and delta wings

    DEESE, J. / AGARWAL, R. / JOHNSON, J. | AIAA | 1991

    Design and test verification of a combustion system for an advanced turbofan engine

    SANBORN, J. / LENERTZ, J. / JOHNSON, J. | AIAA | 1987

    A numerical three-dimensional viscous transonic wing-body analysis and design tool

    MASON, W. / MACKENZIE, D. / STERN, M. et al. | AIAA | 1978

    Evidence of Reynolds number sensitivity in supersonic turbulent shocklets

    JOHNSON, J. A. / ZHANG, Y. / JOHNSON, L. E. | AIAA | 1988

    Development of a class 1.3 minimum smoke propellant

    BIVIN, R. / JOHNSON, J. / MARKOVITCH, I. et al. | AIAA | 1992

    The use of a complex-terrain wind model for the siting and design of wind generators

    YOCKE, M. / JOHNSON, J. / LIU, M.-K. | AIAA | 1979

    Correlation of lift and boundary-layer activity on an oscillating lifting surface

    BASS, R. L. / JOHNSON, J. E. / UNRUH, J. F. | AIAA | 1982

    Analysis of evaporator critical heat flux in the double wall artery heat pipe

    PONNAPPAN, R. / RAMALINGAM, M. / JOHNSON, J. et al. | AIAA | 1988

    MACGS - A zonal grid generation system for complex aero-propulsion configurations

    GATZKE, T. / LABOZZETTA, W. / FINFROCK, G. et al. | AIAA | 1991

    Executive Modular Control of Heterogeneous Spacecraft Components and Agents

    Glass, B. J. / Cannon, H. / Christa, S. et al. | AIAA | 2006

    Advanced turbofan engine combustion system design and test verification

    SANBORN, J. W. / LENERTZ, J. E. / JOHNSON, J. D. | AIAA | 1989

    An Overview of the NASA High Speed ASE Project: Aeroelastic Analyses of a Low-Boom Supersonic Configuration

    Silva, Walter A. / De La Garza, Antonio / Zink, Paul Scott et al. | AIAA | 2015

    A Mechanism for Three-Axis Control of an Ion Thruster Array

    G. S. PERKINS / K. G. JOHNSON / J. D. FERRERA et al. | AIAA | 1972

    Low-Water Plane Multihull Ship Principles, Status, and Plans for Naval Development

    R. Leopold / R. S. Johnson / J. B. Hadler et al. | AIAA | 1973

    Oscillations in digital control systems

    CHENOWETH, D. L. | AIAA | 1971

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