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    Coupled flow, thermal and structural analysis of aerodynamically heated panels (1986)
    In:  CASI
    Details
    Publication Date: 2019-07-20
    Description: A finite element approach to coupling flow, thermal and structural analyses of aerodynamically heated panels is presented. The Navier-Stokes equations for laminar compressible flow are solved together with the energy equation and quasi-static structural equations of the panel. Interactions between the flow, panel heat transfer and deformations are studied for thin stainless steel panels aerodynamically heated by Mach 6.6 flow.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-CR-180687 , NAS 1.26:180687
    Format: application/pdf
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