A Joined-Wing Structural Weight Modeling Study-Reference-Cited by-同舟云学术

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A Joined-Wing Structural Weight Modeling Study

Published:2002-04-22 Issue: Volume: Page:
ISSN:
Container-title:43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
Short-container-title:

Author:

Blair Maxwell Blair¹,Canfield Robert²

Affiliation:

1. Air Force Research Laboratory

2. Air Force Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-1337

Reference15 articles.

1. The joined wing - An overview

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

3. System design innovation using multidisciplinary optimization and simulation

4. Aeroelastic Tailoring of Joined-Wing Configurations

5. Blended-wing-body optimization problem setup

Cited by 31 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. Aero-structural design of joined-wing aircraft based on high-fidelity model;Chinese Journal of Aeronautics;2023-11

2. Flutter Characteristics of a Joined-Wing Unmanned Aerial Vehicle with Variable Dihedral Angles;AIAA Journal;2023-11

3. Aeroelastic Optimization Design of the Global Stiffness for a Joined Wing Aircraft;Applied Sciences;2021-12-12

4. Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future;Progress in Aerospace Sciences;2016-11

5. Buckling Alleviation for Joined-Wing Aircraft;Journal of Aircraft;2016-05

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