Reexamined Structural Design Procedures for Very Flexible Aircraft-Reference-Cited by-同舟云学术

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Reexamined Structural Design Procedures for Very Flexible Aircraft

Published:2014-09 Issue:5 Volume:51 Page:1580-1591
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Cesnik Carlos E.S.¹,Palacios Rafael²,Reichenbach Eric Y.³

Affiliation:

1. Department of Aerospace Engineering, University of Michigan, Ann Arbor, Michigan 48109-2140

2. Department of Aeronautics, Imperial College, London, England SW7 2AZ, United Kingdom

3. Boeing Research and Technology, The Boeing Company, St. Louis, Missouri 63042-2513

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C032464

Reference27 articles.

1. The SensorCraft Configurations: A Non-Linear AeroServoElastic Challenge for Aviation

2. Aeroelasticity of joined-wing airplane configurations - Past work and future challenges - a survey

3. Aeroelasticity of Nonconventional Airplane Configurations-Past and Future

4. Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft

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4. A Sliding-Window Matrix Pencil Method for Aeroelastic Design Optimization with Limit-Cycle Oscillation Constraints;AIAA SCITECH 2024 Forum;2024-01-04

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