Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft-Reference-Cited by-同舟云学术

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Exploration of Optimal Propulsion System Airframe Integration Design Concepts for a Low Boom Supersonic Aircraft

Published:2021-07-28 Issue: Volume: Page:
ISSN:
Container-title:AIAA AVIATION 2021 FORUM
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Author:

Imrak Rumed¹,Karaselvi Emre¹,Tutkun Bulent¹,Nikbay Melike¹

Affiliation:

1. Istanbul Technical University

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2469

Reference27 articles.

1. Nichols, M. R. “Aerodynamics of airframe-engine integration of supersonic aircraft,” NASA Technical Report, 1966.

2. Sonic boom minimization including both front and rear shocks

3. Rodriguez, D., Propulsion/Airframe Integration and Optimization on a Supersonic Business Jet, 2007. https://doi.org/10.2514/ 6.2007-1048, URL https://arc.aiaa.org/doi/abs/10.2514/6.2007-1048.

Cited by 2 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. Redesign of a Low-Boom Supersonic Transport Using Powered Engine Simulation for Sonic Boom Analysis;AIAA SCITECH 2023 Forum;2023-01-19

2. Multi-Fidelity and Multi-Disciplinary Design Optimization of A Low-Boom Supersonic Transport Aircraft;AIAA SCITECH 2023 Forum;2023-01-19

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