Characteristics of the Reacting Flow for the Base‐Bleed Projectile under Dual Stress
Author:
Affiliation:
1. School of Energy and Power Engineering Nanjing University of Science and Technology Nanjing 210094 P.R. China
2. School of Sciences Hangzhou Dianzi University Hangzhou 310018 P.R. China
3. Li Auto Inc. Shanghai 201805 P.R. China
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202100073
Reference29 articles.
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3. Study on acceleration base combustion for low burning rate HTPB propellant;Wan D.;Journal of Solid Rocket Technology,2010
4. Effect of swirl on the regression rate in hybrid rocket motors
5. A. M. Tahsini K. Mazaheri Numerical study of spin acceleration effect on internal ballistics of solid rocket motors.12th Annual Conference of the CFD Society of Canada Ottawa May 9–11 2004.
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