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A performance analysis of the pulsejet intended for aircraft acceleration up to mach number 0,9…1,2
- Authors: Panchenko V.I.1, Borisoglebskij A.V.1
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Affiliations:
- Kazan State Technical University
- Issue: Vol 5, No 2-2 (2006): Special Issue
- Pages: 194-199
- Section: TECHNICAL SCIENCES
- URL: https://journals.ssau.ru/vestnik/article/view/408
- DOI: https://doi.org/10.18287/2541-7533-2006-0-2-2(10)-194-199
- ID: 408
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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
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