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- W811960097 abstract "An axisymmetric mixed-compression supersonic inlet and a single-spool turbojet engine were dynamically tested at Mach 2.5. The propulsion system was subjected to sweep-frequency sinusoidal disturbances of either inlet overboard bypass airflow. The disturbances were at a logarithmic sweep rate of 1 decade per minute. Dynamic responses were taken of signals throughout the propulsion system. Selected signals were reduced relative to the prime propulsion system parameters. The experimental data are presented in Bode plots. Most of the plots are for a frequency range of 1.0 to 50 hertz." @default.
- W811960097 created "2016-06-24" @default.
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- W811960097 date "1972-05-01" @default.
- W811960097 modified "2023-09-27" @default.
- W811960097 title "Dynamics of a supersonic inlet-engine combination subjected to disturbances in fuel flow and inlet overboard bypass airflow" @default.
- W811960097 hasPublicationYear "1972" @default.
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