NASA NTRS · 19750023007
Propulsion systems technology
Abstract
The selection of components, control design, simulation, and tests are examined for designing supersonic propulsion systems. Inlet-engine combination under electronic control are shown. Design and test results from the integrated control for afterburning turbofan and supersonic cruise inlet are presented.
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Hiller, K. W., Batterton, P. G., Burstadt, P. L., Szuch, J. R.. 1975-01-01. Propulsion systems technology. https://ntrs.nasa.gov/citations/19750023007
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