Design Procedure of a Variable Rectangular Inlet for TBCC Engine Considering Mass Flow Requirements
Author:
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42405-024-00725-5.pdf
Reference57 articles.
1. Noh JH, Choi JY, Byun JR, Gil HY, Yoon HG, Lim JS (2010) DARPA’s hypersonic vehicle and TBCC engine programs. J Korean Soc Propul Eng 14(1):65–78
2. Gurijanov EP, Harsha PT (1996) AJAX: new directions in hypersonic technology. In: Space plane and hypersonic systems and technology conference, Norfolk, VA, U.S.A., November 1996, pp 1–9. https://doi.org/10.2514/6.1996-4609
3. Steelant J, Varvill R, Defoort S, Hannemann K, Marini M (2015) Achievements obtained for sustained hypersonic flight within the LAPCAT-II project. In: 20th AIAA international space planes and hypersonic systems and technologies conference, Glasgow, Scotland, July 2015, pp 1–56. https://doi.org/10.2514/6.2015-3677
4. Kojima T, Tanatsugu N, Sato T, Kanda M (2001) Development study on axisymmetric air inlet for ATREX engine. In: 10th AIAA/NAL-NASDA-ISAS international space planes and hypersonic systems and technologies conference, Kyoto, Japan, April 2001, pp 1–8. https://doi.org/10.2514/6.2001-1895
5. Baoxi W, Wenhui L, Feiteng L, Qiang G (2017) Propulsion performance research and status of TRRE Engine experiment. In: 21st AIAA international space planes and hypersonics technologies conference, Xiamen, China, March 2017.https://doi.org/10.2514/6.2017-2351
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