Typical airframe/propulsion interactions such as Mach/altitude excursions and inlet unstarts are reviewed. The improvements in airplane performance and flight control that can be achieved by improving the interfaces between propulsion and flight control are estimated. A research program to determine the feasibility of integrating propulsion and flight control is described. This program includes analytical studies and YF-12 flight tests.
Potential benefits of propulsion and flight control integration for supersonic cruise vehicles
1976-08-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Cooperative Airframe/Propulsion Control for Supersonic Cruise Aircraft
SAE Technical Papers | 1974
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