Experiments on the Heat Transfer and on the Aerodynamic Coefficients of a Delta Wing in Rarefied Hypersonic Flows

Author:

Chun Ch.-H.

Publisher

Springer Berlin Heidelberg

Reference9 articles.

1. A Stanbrook, L.C. Squire, Possible Types of Flow at Swept Leading Edges. The Aeronautical Quarterly, Vol. 15, Feb. 1964, pp. 72–82.

2. DJ. Peake, M. Tobak, Three-Dimensional Interactions and Vortical Flows With Emphasis on High Speeds. AGARDograph No. 252, July 1980.

3. E.J. Cross, Jr., Experimental and Analytical Investigation of the Expansion Flow Field Over a Delta Wing at Hypersosnic Speeds. ARL 68-0027, Feb. 1968, Report of Aerospace Research Laboratories (ARL ), US Air Force.

4. K.Y. Narayan, Lee Side Flow Field and Heat Transfer of a Delta Wing at Ma∞= 10. AIAA Journal, Vol. 16, No. 2, pp. 160–165, Feb. 1978.

5. D.M. Rao, A.H. Whiteheard, Jr., Lee-Side Vortices on Delta Wing at Hypersonic Speeds. AIAA Journal, Vol. 10, Nov. 1972, pp. 1458–1465.

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