THERMAL BOUNDARY LAYER IN SLIP FLOW REGIME

descriptionPublicationkeyboard_double_arrow_right Article 01 Oct 1963 English Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:AIAA Journal, volume 1, pages 2,396-2,398 (issn: 0001-1452, eissn: 1533-385X,

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Authors: Reddy, K. C.;

doi: 10.2514/3.2078

THERMAL BOUNDARY LAYER IN SLIP FLOW REGIME

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Abstract

5 Petrick, E. N. and Krauss, J. J., "The design and evaluation of perforated ion emitters" Final TR, Contract AF 33(657)-8638, performed for Aeronaut. Systems Div., U. S. Air Force, by Kelsey Hayes Co., Romulus, Mich. (September 15, 1963). 6 Winterbottom, W. L. and Hirth, J. P., "Diffusional contribution to the total flow from a knudsen cell," J. Chem. Phys. 37, 784-793 (1962). formation (2), Eq. (4.3) becomes

Related Organizations

Indian Institute of Technology Kharagpur
India

Keywords

fluid mechanics

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