Effect of Differential Sweep on a Three-Dimensional Sidewall-Type Intake at Mach 3.5
Author:
Publisher
Springer International Publishing
Link
http://link.springer.com/content/pdf/10.1007/978-3-319-46213-4_35
Reference6 articles.
1. Trexlar, C.A.: Inlet performance of integrated Langley scramjet module. AIAAPaper No. 75–121, Sept-Oct 1975
2. Smart, M., Trexlar, C.A.: Mach 4 performance of fixed geometry hypersonic inlet with rectangular to elliptic shape transition. 41st Aerospace Science Meeting and Exhibit AIAA 2003-12
3. Holland, S.D.: Mach 10 Computational study of three dimensional scramjet flow field. NASA TM 4602, 1995
4. Kumar, A., Trexlar, C.A.: Numerical study of the effect of the reverse sweep on scramjet inlet performance. J. Propul. Power 8 (3), pp. 714–719 (1992)
5. Watanabe, Y., Murakami, A., Fujiwara, H.: Effect of sidewall configuration on the aerodynamic performance of the supersonic air-intake. AIAA 2002-3777
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