Aeroelastic Analysis Using FUN3D-Based ROM Simultaneously Subject to Gust and Control Surface Deflections-Reference-Cited by-同舟云学术

Aeroelastic Analysis Using FUN3D-Based ROM Simultaneously Subject to Gust and Control Surface Deflections

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
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Author:

Wang Zhicun¹,Yang Shuchi¹,Chen Ping-Chih¹

Affiliation:

1. ZONA Technology, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1021

Reference11 articles.

1. Unified Aeroelastic and Flight Dynamic Formulation via Rational Function Approximations

2. A Compact CFD-Based Reduced Order Modeling for Gust Analysis

3. Nonlinear Gust Reduced Order Modeling Based On FUN3D And Volterra Theory

4. An Efficient Euler Method on Non-Moving Cartesian Grids with Boundary-Layer Correction for Wing Flutter Simulations

5. Bartels, R.E. "Development, Verification and Use of Gust Modeling in the NASA Computational Fluid Dynamics Code FUN3D". 2012, NASA.NASA/TM-2012-217771.

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