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Results of an experimental and numerical study of the aerodynamic heating of the undersurface of delta wings with sharp leading edges at mach numbers M∞=6.1 and 8

✍ Scribed by N. A. Kovaleva; N. P. Kolina; A. P. Kosykh; A. Ya. Yushin


Publisher
Springer
Year
1992
Tongue
English
Weight
473 KB
Volume
26
Category
Article
ISSN
0015-4628

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