Environmental MDO and Uncertainty Hybrid Approach Applied to a Supersonic Business Jet-Reference-Cited by-同舟云学术

Environmental MDO and Uncertainty Hybrid Approach Applied to a Supersonic Business Jet

Published:2008-06-14 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
language:
Short-container-title:

Author:

Deremaux Yann¹,Pietremont Nicolas¹,Negrier Jean¹,Herbin Erick¹,Ravachol Michel¹

Affiliation:

1. Dassault Aviation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-5832

Reference19 articles.

1. Net thrust 22074 23493 +6.4% Cumulative noise

2. BFL 1920 m 1890 m -1.5% Emission index 8 8 stable

3. EW 23252kg 24645kg +6% 24645kg +6% Fuel Weight 26730kg 29460kg +10.2% 27200kg +1.8% Wingarea 148 m² 155.7 m² +5.2% 155.7 m² +5.2% Netthrust 22074daN 23722daN +7.5% 23722daN +7.5%

4. BFL 6300ft 6400ft +1.5% 6185ft -2% Emission index 9 9.9 +10% 8.6 -4.5%

Cited by 6 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. Two-Level Approach for Simultaneous Component Assignment and Layout Optimization with Applications to Spacecraft Optimal Layout;Applied Sciences;2024-09-10

2. Hidden-variables genetic algorithm for variable-size design space optimal layout problems with application to aerospace vehicles;Engineering Applications of Artificial Intelligence;2023-05

3. Multidisciplinary Design Optimization of Low-Boom Supersonic Aircraft with Mission Constraints;AIAA Journal;2021-01

4. Application of Multi-disciplinary Design Optimization in Manned Submersible Design;Ocean Engineering & Oceanography;2020

5. Shape optimization of an airfoil in a BZT flow with multiple-source uncertainties;Computer Methods in Applied Mechanics and Engineering;2011-01