INVENT Surrogate Modeling and Optimization of Transient Thermal Responses-Reference-Cited by-同舟云学术

INVENT Surrogate Modeling and Optimization of Transient Thermal Responses

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Miller Cameron¹,Maser Adam²,Garcia Elena²,Mavris Dimitri²

Affiliation:

1. Lockheed Martin Corporation

2. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-1123

Reference6 articles.

1. INVENT Modeling, Simulation, Analysis and Optimization

2. Generic Aircraft Thermal Tip-to-Tail Modeling and Simulation

3. 4modeFRONTIER,SoftwarePackage,Ver.4.3.0,ESTECO,Trieste,Italy,2010.

4. 5Phan, L. L. "A Methodology for the Efficient Integration of Transient Constraints in the Design of Aircraft Dynamic Systems," Ph.D. Thesis, Schoolof Aerospace Engineering,Georgia InstituteofTechnology, Atlanta, GA,2010.

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