Wake Measurements on Blended Wing Body with Gurney Flaps in Low Speed Flows-Reference-Cited by-同舟云学术

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Wake Measurements on Blended Wing Body with Gurney Flaps in Low Speed Flows

Published:2019-01-06 Issue: Volume: Page:
ISSN:
Container-title:AIAA Scitech 2019 Forum
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Author:

Yamada Tatsuya¹,Taguchi Masato¹,Duong Nguyen Thai¹,Kashitani Masashi¹,Kusunose Kazuhiro¹,Takita Yoshihiro¹

Affiliation:

1. National Defense Academy

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1617

Reference17 articles.

1. https://www.nasa.gov/centers/langley/factsheets/FS-2003-11-81-LaRC.html

2. Extension of Wake-Survey Analysis Method to Cover Compressible Flows

Cited by 4 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. Computational Investigation of A Blended Wing Body at Low Speeds;Journal of Aerospace Sciences and Technologies;2023-07-25

2. Recent developments of blended wing body aircraft: experimental, numerical and theoretical approaches;Aerospace Systems;2022-03-07

3. Analysis of a Wing–Fuselage Biplane with Trailing-Edge Flaps in Low-Speed Flow;Journal of Aircraft;2021-09-25

4. Aerodynamic Characteristics of Busemann Biplane by Wake Measurements in Low-Speed Wind Tunnel;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2021

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