High-Fidelity Aerostructural Design Optimization of a Supersonic Business Jet-Reference-Cited by-同舟云学术

High-Fidelity Aerostructural Design Optimization of a Supersonic Business Jet

Published:2004-05 Issue:3 Volume:41 Page:523-530
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Martins Joaquim R. R. A.¹,Alonso Juan J.²,Reuther James J.³

Affiliation:

1. University of Toronto Institute for Aerospace Studies, Toronto, Ontario M3H 5T6, Canada

2. Stanford University, Stanford, California 94305

3. NASA Ames Research Center, Moffett Field, California 95035

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.11478

Reference23 articles.

1. Multidisciplinary aerospace design optimization: survey of recent developments

2. 3Wakayama, S. R. "Lifting Surface Design Using Multidisciplinary Optimization," Ph.D. Dissertation,Dept. of Aeronautics and Astronautics, Stanford Univ., Stanford, CA,Dec. 1994.

3. AEROELASTIC CHALLENGES FOR A HIGH SPEED CIVIL TRANSPORT

4. A novel sensitivity analysis method for high fidelity multidisciplinary optimization of aero-structural systems

Cited by 197 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. Electrothermal Coupling Methodologies and Their Influence on the Optimization of Aircraft Electric Motors;AIAA Journal;2024-07

2. MachLine: Development of a Dirichlet-Based, Subsonic/Supersonic Panel Method for Unstructured Grids;Journal of Aircraft;2024-07

3. Aerodynamic design optimization of a NACA 0012 airfoil: An introductory adjoint discrete tool for educational purposes;International Journal of Mechanical Engineering Education;2024-05-21

4. Multiobjective aerostructural optimization for efficient transport wing conceptual design;Aerospace Science and Technology;2024-05

5. Discrete and Continuous Adjoint-Based Aerostructural Wing Shape Optimization of a Business Jet;Fluids;2024-04-05