Development-Fluid-Dynamics-Based Aerothermoelastic Simulation Capability with Application to Flight Vehicles-Reference-Cited by-同舟云学术

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Development-Fluid-Dynamics-Based Aerothermoelastic Simulation Capability with Application to Flight Vehicles

Published:2016-03 Issue:2 Volume:53 Page:360-368
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Gupta K. K.¹,Choi S. B.²,Ibrahim H.³

Affiliation:

1. NASA Armstrong Flight Research Center, Edwards, California 93523

2. Department of Mechanical Engineering, California State University, Los Angeles, Los Angeles, California 90032

3. Department of Engineering, Norfolk State University, Norfolk, Virginia 23504

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033346

Reference23 articles.

1. Euler solutions for transonic flow past a fighter wing

2. Aeroelastic analysis of wings using the Euler equations with a deforming mesh

3. Lee-RauschE. M.BatinaJ. T. “Wing Flutter Boundary Prediction Using Unsteady Euler Aerodynamic Method,” NASA TM-107732, March 1993.

4. Unsteady Euler algorithm with unstructured dynamic mesh for complex-aircraft aerodynamic analysis

5. Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerothermoelastic Analysis and Optimization of Stiffened Thin-Walled Structures;AIAA SCITECH 2022 Forum;2022-01-03

2. A High-Fidelity Coupling Framework for Aerothermoelastic Analysis and Adjoint-Based Gradient Evaluation;AIAA Scitech 2021 Forum;2021-01-04

3. Correction: Development of a Fluid-Dynamics-Based Aerothermoelastic Simulation Capability with Application to Flight Vehicles;Journal of Aircraft;2020-11

4. A Study on the Structural Integrity of Hypersonic Vehicles According to Flight Conditions;Journal of the Korean Society for Aeronautical & Space Sciences;2019-10-31

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