A Parametric and Physics-Based Approach to Structural Weight Estimation of the Hybrid Wing Body Aircraft-Reference-Cited by-同舟云学术

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A Parametric and Physics-Based Approach to Structural Weight Estimation of the Hybrid Wing Body Aircraft

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Laughlin Trevor¹,Corman Jason¹,Mavris Dimitri¹

Affiliation:

1. Georgia Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1082

Reference28 articles.

1. Design of the Blended Wing Body Subsonic Transport

2. Hybrid Wing Body Configuration System Studies

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2. Certification-Driven Platform for Multidisciplinary Design Space Exploration in Airframe Preliminary Design;Journal of Aircraft;2021-10-20

3. Structural Optimization of Blended Wing Body Transport Aircraft With Buckling Constraints;AIAA AVIATION 2021 FORUM;2021-07-28

4. A Study on Various Mesh Generation Techniques used for Engineering Applications;Journal of Innovative Image Processing;2021-06-02

5. Aerodynamic design of integrated propulsion–airframe configuration of a hybrid wing body aircraft;Shock Waves;2019-11

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