Mass flow rate effect on a rotating detonation combustor with an axial air injection
Author:
Funder
National Energy Technology Laboratory
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00193-020-00984-7.pdf
Reference42 articles.
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2. Rankin, B.A., Richardson, D.R., Caswell, A.W., Naples, A.G., Hoke, J.L., Schauer, F.R.: Chemiluminescence imaging of an optically accessible non-premixed rotating detonation engine. Combust. Flame 176, 12–22 (2017). https://doi.org/10.1016/j.combustflame.2016.09.020
3. Wolański, P.: Application of the continuous rotating detonation to gas turbine. In: Applied Mechanics and Materials, vol. 782. Trans Tech Publications, pp. 3–12 (2015). https://doi.org/10.4028/www.scientific.net/AMM.782.3
4. Wolański, P., Kalina, P., Balicki, W., Rowiński, A., Perkowski, W., Kawalec, M., Łukasik, B.: Development of gasturbine with detonation chamber. In: Li, J.M., Teo, C.J., Khoo, B.C., Wang, J.P., Wang, C. (eds.) Detonation Control for Propulsion. Springer, Cham, pp. 23–37 (2018). https://doi.org/10.1007/978-3-319-68906-7_2
5. Bykovskii, F.A., Zhdan, S.A., Vedernikov, E.F.: Continuous spin detonations. J. Propul. Power 22(6), 1204–1216 (2006). https://doi.org/10.2514/1.17656
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