Analysis of a Compressible Laminar Boundary Layer on a Yawed Cone
Author:
Affiliation:
1. Institutde Mecanique des Fluides de Marseille, Marseille, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.61442
Reference16 articles.
1. Laminar boundary layer on a cone at incidence in supersonic flow
2. 3Murdock, W. "The Solution of Sharp Cone Boundary Layer Equations in the Plane of Symmetry,*' Journal of Fluid Mechanics, Vol.54, Pt. 4,1972, pp.665-678.
3. 4Lin, T. C. and Rubin, S. G. "Viscous Flow Over a Cone at Moderate Incidence, Part II: Supersonic Boundary Layer," Rept. 72-27,Sept. 1972, Polytechnic Inst. of Brooklyn, Aerodynamics Lab.
4. also Journal of Fluid Mechanics, Vol.59, Pt. 3, July 1973, pp.593-620.
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Calculation of a laminar boundary layer on the leeward side of a triangular plate with supersonic leading edges;Journal of Applied Mechanics and Technical Physics;1989
2. Laminar boundary layers on slightly-inclined nearly-circular supersonic cones;20th Aerospace Sciences Meeting;1982-01-11
3. Turbulent Surface Flow around a Yawed Cone;AIAA Journal;1978-08
4. Heat transfer—a review of 1976 literature;International Journal of Heat and Mass Transfer;1977-11
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