A Methodology for Coupled Thermal-Structural Analysis and Structural Design of Scramjet Combustor

Author:

Purwar Anupam,Mahapatra D. Roy,Thakor Nimesh,Priyamvada K. S.,Mukherjee Ragini

Publisher

Springer International Publishing

Reference18 articles.

1. Thornton, E.A., Dechaumphai, P.: Coupled flow, thermal, and structural analysis of aerodynamically heated panels. J. Aircraft 25(11), 1052–1059 (1988)

2. Culler, A.J., McNamara, J.J.: Fluid-thermal-structural modeling and analysis of hypersonic structures under combined loading. In: 52nd AIAA Structures, Structural Dynamics and Materials Conference, 2011

3. Ho, S.-Y., Paull, A.: Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test. Aerosp. Sci. Technol. 10(5), 420–426 (2006)

4. Ho, S.-Y., Kotousov, A., Nguyen, P., Harding, S., Codrington J., Tsukamoto, H.: FGM (Functionally Graded Material) Thermal Barrier Coatings for Hypersonic Structures – Design and Thermal Structural Analysis, Source: http://www.dtic.mil/dtic/tr/fulltext/u2/a474097.pdf , Accessed Oct 2014

5. Sobotka, J.C., Oral, A., Culler, A.J.: Towards a coupled loads-response-life prediction framework for hypersonic structures in combined extreme environments. In: 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2013

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