Export to Refworks Export to EndNote Email
Report an Issue

Coupled flow, thermal and structural analysis of aerodynamically heated panels

Author:
Thornton, Earl A.
Published:
Mar 1, 1986.
Physical Description:
1 electronic document
Additional Creators:
Dechaumphai, Pramote
Online Version

Availability

I Want It

Finding items...

Restrictions on Access:
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary:
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.
Other Subject(s):
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 19870017693.
Accession ID: 87N27126.
NAS 1.26:180687.
NASA-CR-180687.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15697855