Uniform second-order solution for supersonic flow over delta wing using reverse-flow integral method
نویسندگان
چکیده
منابع مشابه
Analytic Solution for Hypersonic Flow Past a Slender Elliptic Cone Using Second-Order Perturbation Approximations
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ژورنال
عنوان ژورنال: Journal of Fluid Mechanics
سال: 1964
ISSN: 0022-1120,1469-7645
DOI: 10.1017/s0022112064000179