Prediction of Heat Transfer From Laminar Boundary Layers, With Emphasis on Large Free-Stream Velocity Gradients and Highly Cooled Walls

Author:

Back L. H.1,Witte A. B.1

Affiliation:

1. Research and Advanced Concepts Section, Jet Propulsion Laboratory, Pasadena, Calif.

Abstract

Laminar boundary-layer heat transfer and shear-stress predictions from existing similarity solutions are extended in an approximate way to perfect gas flows with a large free-stream velocity gradient parameter β and variable density-viscosity product ρμ across the boundary layer resulting from a highly cooled wall. The dimensionless enthalpy gradient at the wall gw′, to which the heat flux is related, is found not to vary appreciably with β. Thus the application of similarity solutions on a local basis to predict heat transfer from accelerated flows to an arbitrary surface may be a reasonable approximation involving a minimum amount of calculation time. Unlike gw′, the dimensionless velocity gradient at the wall fw″, to which the shear stress is related, is strongly dependent on β.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Cited by 21 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

1. Compressible Boundary-Layer Theory;Analytical Fluid Dynamics, Second Edition;2000-12-21

2. Laminar boundary layers with vectored mass transfer;International Journal of Engineering Science;1987-01

3. Experimental Determination of the Discharge Coefficients for Critical Flow through an Axisymmetric Nozzle;AIAA Journal;1978-01

4. Discharge coefficient of a chemical laser nozzle;AIAA Journal;1977-01

5. References and Author Index;Applied Mathematics and Mechanics;1974

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