This document is intended as a progress report on fluidics as applied to aerospace propulsion problems. After a minimal review of basic operating principles, a number of operating prototype sensors and control systems will be described. Fluidic control systems for aerodynamic inlets, gas turbines, and rocket engines will be treated. Some of these systems have functioned successfully at temperatures exceeding 3000 Kelvin. (Author)


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    Aerospace propulsion systems

    Ward, Thomas A. ;Ward, Thomas Arthur | SLUB | 2010


    Aerospace propulsion systems

    Ward, Thomas A. / Ward, Thomas Arthur | TIBKAT | 2010



    Fluidic Applications in Aerospace

    John M. Goto | AIAA | 1978