Integrated Variable-Fidelity Tool Set for Modeling and Simulation of Aeroservothermoelasticity-Propulsion (ASTE-P) of Aerospace Vehicles from Subsonic to Hypersonic-Reference-Cited by-同舟云学术

Integrated Variable-Fidelity Tool Set for Modeling and Simulation of Aeroservothermoelasticity-Propulsion (ASTE-P) of Aerospace Vehicles from Subsonic to Hypersonic

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
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Author:

Hu Patrick¹,Xue Liping¹,Ni Kan¹,Brenner Martin²

Affiliation:

1. Advanced Dynamics Inc.

2. DFRC

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6141

Reference26 articles.

1. Fluid-membrane interaction based on the material point method

2. Flip: A low-dissipation, particle-in-cell method for fluid flow

3. Application of a particle-in-cell method to solid mechanics

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