Supersonic Bi-Directional Flying Wing Configuration with Low Sonic Boom and High Aerodynamic Efficiency-Reference-Cited by-同舟云学术

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Supersonic Bi-Directional Flying Wing Configuration with Low Sonic Boom and High Aerodynamic Efficiency

Published:2011-06-27 Issue: Volume: Page:
ISSN:
Container-title:29th AIAA Applied Aerodynamics Conference
language:
Short-container-title:

Author:

Berger Clemence¹,Carmona Kevin¹,Espinal Daniel¹,Im Hongsik¹,Zha Gecheng¹

Affiliation:

1. University of Miami

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3663

Reference50 articles.

1. Sonic Boom Research: History and Future (Invited)

2. The oblique wing—aircraft design for transonic and low supersonic speeds

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. Review of Sonic Boom Prediction and Reduction Methods for Next Generation of Supersonic Aircraft;Aerospace;2023-10-27

2. Feasibility of Supersonic Aircraft Concepts for Low-Boom and Flight Trim Constraints;33rd AIAA Applied Aerodynamics Conference;2015-06-19

3. Near field Sonic Boom calculation of Benchmark Cases;53rd AIAA Aerospace Sciences Meeting;2015-01-03

4. Analysis of a Low Boom Supersonic Flying Wing Preliminary Design;53rd AIAA Aerospace Sciences Meeting;2015-01-03

5. Parametric Trade Study for Supersonic Bi-Directional Flying Wing;32nd AIAA Applied Aerodynamics Conference;2014-06-13

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