Influence of a reverse delta-type add-on device on wake vortex alleviation
Particle image velocimetry was used in a low-speed wind tunnel to investigate the effect of interactions of vortices produced by a wingtip of a half-span wing (NACA 23012 in landing configuration) and a slender reverse delta-type add-on device placed near the tip on the upper surface of the half-spa...
保存先:
| 主要な著者: | , , , |
|---|---|
| フォーマット: | 論文 |
| 言語: | English English English |
| 出版事項: |
American Institute of Aeronautics and Astronautics Inc. (AIAA)
2016
|
| 主題: | |
| オンライン･アクセス: | http://irep.iium.edu.my/53914/9/53914_Influence%20of%20a%20Reverse%20Delta-Type_new%20text.pdf http://irep.iium.edu.my/53914/10/53914_Influence%20of%20a%20Reverse%20Delta-Type.pdf_WOS.pdf http://irep.iium.edu.my/53914/11/53914_Influence%20of%20a%20Reverse%20Delta-Type.pdf_SCOPUS.pdf http://irep.iium.edu.my/53914/ https://arc.aiaa.org/doi/pdf/10.2514/1.J054436 |
| タグ: |
タグ追加
タグなし, このレコードへの初めてのタグを付けませんか!
|
インターネット
http://irep.iium.edu.my/53914/9/53914_Influence%20of%20a%20Reverse%20Delta-Type_new%20text.pdfhttp://irep.iium.edu.my/53914/10/53914_Influence%20of%20a%20Reverse%20Delta-Type.pdf_WOS.pdf
http://irep.iium.edu.my/53914/11/53914_Influence%20of%20a%20Reverse%20Delta-Type.pdf_SCOPUS.pdf
http://irep.iium.edu.my/53914/
https://arc.aiaa.org/doi/pdf/10.2514/1.J054436