Mechanism of adjusting bypass ratio by front variable area bypass injector for a variable cycle engine
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Elsevier BV
Reference23 articles.
1. Kurzke J. The mission defines the cycle: turbojet, turbofan and variable cycle engines for high speed propulsion. Brussels: NATO; 2010. Report No.: ADA596249.
2. Johnson JE. Variable cycle engines─The next step in propulsion evolution. Reston: AIAA; 1976. Report No.: AIAA-1976-0758.
3. Johnson JE. Variable cycle engine developments at general electric-1955-1995. In: Murthy SNB, Curran ET, editors. Developments in high-speed vehicle propulsion systems. Reston: AIAA; 1996. p. 105–58.
4. Bartolotta PA, McNelis NB, Shafer DG. High speed turbines: Development of a turbine accelerator (RTA) for space access. Reston: AIAA; 2003. Report No.: AIAA-2003-6943.
5. Aircraft propulsion;Farokhi,2014
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