Matching mechanism analysis on an adaptive cycle engine

Author:

Zheng Junchao,Chen Min,Tang Hailong

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference17 articles.

1. Kurzke J. The mission defines the cycle: turbojet, turbofan and variable cycle engines for high speed propulsion. NATO; 2010. Report No.: RTO Educational Notes, EN-AVT-185 Lecture.

2. Peter V, Walter B. Study of an airbreathing variable cycle engine. Reston: AIAA; 2011. Report No.: AIAA-2011-5758.

3. Simmons R. J. Design and control of a variable geometry turbofan with an independently modulated 3rd stream[dissertation]. Columbus, Ohio: Ohio State University; 2009.

4. GE Co., Aerodynamic/acoustic performance of YJ101/double bypass VCE with cannular plug nozzle. Washington, D.C.: NASA; 1981. Report No.: NASA-CR-159869.

5. Steady performance investigation at various modes of an adaptive cycle aero-engine;Li;J Propul Technol,2013

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