Numerical Modeling of the RDE
Author:
Affiliation:
1. Principal Research Engineer, Gexcon AS , Norway
2. Senior Technical Expert, SST SwissSafeTech AG , Switzerland
3. Łukasiewicz Research Network – Institute of Aviation , Al. Krakowska 110/114, 02-256 Warsaw
Abstract
Publisher
Walter de Gruyter GmbH
Link
https://www.sciendo.com/pdf/10.2478/tar-2020-0019
Reference41 articles.
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2. [2] Shao, Y.-T., Liu, M. and Wang, J.-P., 2010, “Numerical Investigation of Rotating Detonation Engine Propulsive Performance,” Combustion Science and Technology, 182(11-12), pp. 1586-1597. 10.1080/00102202.2010.497316.
3. [3] Yetao, S., Meng, L. and Jianping, W., 2010, “Continuous Detonation Engine and Effects of Different Types of Nozzle on Its Propulsion Performance,” Chinese Journal of Aeronautics, 23(6), pp. 647-652. 10.1016/S1000-9361(09)60266-1.
4. [4] Liu, S.-J., Lin, Z.-Y., Sun, M.-B. and Liu, W.-D., 2011, “Thrust Vectoring of a Continuous Rotating Detonation Engine by Changing the Local Injection Pressure,” Chinese Physics Letters, 28(9), p. 094704. 10.1088/0256-307x/28/9/094704.
5. [5] Liu, M., Zhou, R. and Wang, J.-P., 2011, “Three-dimensional simulation of rotating detonation engines,” presented at the IWDE, Tokyo.
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