Survey of general requirements for performance and control of supersonic inlets for turbojet or turbofan propulsion systems for supersonic transport; interaction between inlet and engine performance are considered and effects of pressure recovery, bleed flows, and external drags on engine thrust and specific fuel consumption for design and off-design operation; problem of controlling inlet to obtain safe and efficient operation; effects of control tolerances on inlet geometry and terminal shock position on engine performance are also shown; possible approaches for simplifying or improving inlet control system.
Engine air inlet compatibility for supersonic transport
SAE -- Paper
SAE Meeting ; 1965 Inlets
1965
34 pages
Conference paper
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Engine Air Inlet Compatibility for the Supersonic Transport
SAE Technical Papers | 1965
|Inlet Duct—Engine Airflow Match and Compatibility for Supersonic Aircraft
SAE Technical Papers | 1962
|Inlet duct -- Engine airflow match and compatibility for supersonic aircraft
Engineering Index Backfile | 1962
|