Author:
Smith A. G.,Spalding D. B.
Abstract
A simple method is given for the calculation of the heat transfer from a laminar flow surface. Computation is by a quadrature. The method is essentially a simplification and extension of the Eckert(1) method, and is applicable both to two–dimensional and to axisymmetric flows.
Publisher
Cambridge University Press (CUP)
Reference11 articles.
1. Contributions to the theory of heat transfer through a laminar boundary layer
2. Approximate Calculation of the Laminar Boundary Layer
3. Walz A. (1941). Ein neuer Ansatz für das Geschwindigkeitsprofil der laminaren Reibungsschicht. Lilienthal Bericht 141, 8, 1941.
4. Young A. D. and Winterbottom N. E. (1942). Note on the Effect of Compressibility on the Profile Drag of Aerofoils in the Absence of Shock Waves. R. & M. 2068, 1942.
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