Performance Analysis of Propulsion Powered by Rotating Detonation Rocket Based Combined Cycle (RDRBCC)
Performance Analysis of Propulsion Powered by Rotating Detonation Rocket Based Combined Cycle (RDRBCC)
Author
Wang, Bing
International Society for Air Breathing Engines
Xie, Qiaofeng
Date
2015-10-22
Item Type
Degree Name
Academic Department
Identifiers
20145
Keywords
Subject
Systems: Combined cycle engines
Publisher Link
Abstract
Description
This paper is part of the conference proceedings from the 22nd International Symposium on Air Breathing Engines.