Structural Optimization of Flight Vehicles with Computational-Fluid-Dynamics-Based Maneuver Loads

Author:

Raveh Daniella E.1,Karpel Mordechay1

Affiliation:

1. Technion—Israel Institute of Technology, Haifa 32000, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 25 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. Computational Study of Transonic Limit Cycle Oscillation Phenomenon on F-16 Fighter Aircraft;Journal of Aircraft;2017-03

2. An airplane jig shape design method based on high fidelity aeroelastic simulation;Aerospace Science and Technology;2015-12

3. Generalized Approach to Aeroelastic CFD Time Simulation of Morphing Flight Vehicles;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

4. Computational Aeroelasticity Research in Israel;50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2009-05-04

5. Computational Aeroelastic Simulation of Rapidly Morphing Wing-Body Configurations;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07

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