Three-dimensional stagnation-point heat transfer in equilibrium air flows

Author:

WORTMAN ANDRZEJ1

Affiliation:

1. Northrop Corporation, Hawthorne, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference8 articles.

1. Poots, G. "Compressible Laminar Boundary-Layer Flow at a Point of Attachment/' Journal of Fluid Mechanics, Vol.22, Pt. 1,1965, pp.197-208.

2. Heat and mass transfer at a general three- dimensional stagnation point.

3. Cohen, N. R, "Boundary-Layer Similar Solutions and Correlation Equations for Laminar Heat Transfer Distribution in Equilibrium Air at Velocities up to 41,100 Feet per Second," TR-118,1961, NASA.

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1. Boundary layer flow at a three-dimensional stagnation point in power-law non-Newtonian fluids;International Journal of Heat and Fluid Flow;1993-12

2. A numerical technique for three-dimensional compressible boundary layers;International Journal for Numerical Methods in Fluids;1985-02

3. An application of Keller's method to the solution of an eighth-order nonlinear boundary value problem;International Journal for Numerical Methods in Engineering;1980-08

4. Heat and Mass Transfer at a General Three-Dimensional Stagnation Point;AIAA Journal;1975-06

5. Heat transfer—A review of 1971 literature;International Journal of Heat and Mass Transfer;1972-11

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