Abstract
SummaryA theory is presented describing the flow close to the surface of a circular cone at incidence to a supersonic stream, which reconciles the first order theory of Stone (on which the widely used M.I.T. Cone Tables are based) with the physically necessary condition that the entropy on the cone surface be constant.However, the results of this “vortical layer” solution appear to invalidate the method used in Ref. 1 to apply a boundary condition at the cone surface, and so to cast doubt on the results obtained by this theory.
Publisher
Cambridge University Press (CUP)
Reference9 articles.
1. Woods B. A. Unpublished College of Aeronautics Thesis, 1956.
2. Cheng H. K. Hypersonic Shock-Layer Theory of a Yawed Cone and Other Three- Dimensional Pointed Bodies. Wright Air Development Center Technical Note 59-335 and A.R.C. 22,076, October 1959.
3. On Supersonic Flow Past a Slightly Yawing Cone II
4. Ferri A. Supersonic Flow Around Circular Cones at Angles of Attack. N.A.C.A. Report 1045, 1951.
5. The air pressure on a cone moving at high speeds.—I
Cited by
8 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