Free-Jet Testing of a Supersonic Engine/Intake Combination
- 1 March 1970
- journal article
- symposium on-altitude-testing
- Published by Cambridge University Press (CUP) in The Aeronautical Journal
- Vol. 74 (711) , 212-218
- https://doi.org/10.1017/s000192400011396x
Abstract
The design and development of aircraft powerplants for sustained supersonic operation proves to be an exacting task which involves careful balancing of the requirements for high installed performance and system viability. The latter question may be dominated by the need to ensure flow compatibility at the intake/engine interface.Keywords
This publication has 3 references indexed in Scilit:
- Design and development of an air intake for a supersonic transport aircraft.Journal of Aircraft, 1968
- Olympus in Concord - The tools of developmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- Propulsion Controls on the ConcordeJournal of the Royal Aeronautical Society, 1966