A performance analysis of the pulsejet intended for aircraft acceleration up to mach number 0,9…1,2

Abstract


It was investigated and optimized pulsejet`s performances. As compared with other flying analogues the engine is available flying up to 0,9…1,2 Mach number. The pulsejet could be used as propulsion system for high-speed unmanned aircraft, as space vehicle’s first-stage engine.


About the authors

V. I. Panchenko

Kazan State Technical University

Author for correspondence.
Email: sadohina@ssau.ru

Russian Federation

A. V. Borisoglebskij

Kazan State Technical University

Email: sadohina@ssau.ru

Russian Federation

References

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