Engine-demand airflow used as primary control parameter. Optimum inlet angle depends on such other variables as mach number, altitude, and ambient temperature. Function of these variables approximated by schedule ("inlet ramp schedule") of digitized values implemented by digital control system.
Universal Controller For Supersonic Engine Inlet
NASA Tech Briefs ; 19 , 8
1995-08-01
Miscellaneous
No indication
English
Universal Controller for Supersonic Engine Inlet
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