Estimation of aerodynamic heat transfer in free flight at Mach number up to 4.7

Author:

Mehta R. C.

Publisher

Springer Science and Business Media LLC

Subject

General Engineering

Reference15 articles.

1. Rumsey, C. B.; Lee, D. B.: Measurements of aerodynamic heat transfer on a 15° cone-cylinder. Flare configuration in free flight at Mach numbers upto 4.7. NASA TN D-824, Langley Research Centre, May 1961

2. Burggraf, O. R.: An exact solution of the inverse problem in heat conduction theory and applications. J. Heat Transfer 82 (1964)378–382

3. Stolz, G.: Numerical solutions of an inverse problem of heat conduction for simple shapes. J. Heat Transfer 82 (1960) 20–26

4. Beck, J. V.: Surface heat flux determination using an integral method. Nucl. Eng. Des. 7 (1968) 170–178

5. Sparrow, E. M.; Haji-Sheikh, A.; Lundgren, T. S.: The inverse problem in transient heat conduction. J. Appl. Mech. 86(1964)369–375

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