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ISSN Online: 2377-424X

International Heat Transfer Conference 4
August 31 - September 5, 1970, Paris-Versailles, France

LAMINAR HEAT TRANSFER CALCULATION ON CONICAL BODIES IN SUPERSONIC FLOW

Get access (open in a dialog) DOI: 10.1615/IHTC4.2290
pages 1-11

Abstract

The laminar boundary-layer development on conical bodies of arbitrary cross section is calculated with a method of solution based on quasi-linearization and an implicit finite-difference method. Boundary conditions include arbitrary circumferential distribution of wall temperature, heat transfer, and blowing or suction. Fluid-property options are perfect gas or real gas in equilibrium.

Sample calculations that make use of exact inviscid solutions, are given for circular cones. The main results are circumferential shear stress and heat-transfer distributions showing the effects of wall temperature, blowing and suction, angle of attack and cone half-angle.