Numerical Investigation of Aircraft High-speed Runway Exit Using Generalized Optimal Control (AIAA 2018-0879)
Guidance, navigation and control (Conference)
01.01.2018
17 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Numerical Investigation of Inlet Injection in a Rotating Detonation Engine (AIAA 2015-0879)
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2018
|