Abstract
Abstract The possibility of supersonic flight in turbojet-powered aircraft is shown, and the resulting thrust requirements for the engine are estimated. The performance requirements of a turbojet installation are considered from the point of view of an aerodynamicist. Afterburning, inlet-pressure recovery and drag, matching of inlet size and engine, and the effect of exit and cooling losses are considered. Speed stability and jet problems are discussed briefly.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
