Effect of Passive Bleeding on Flow Structure over a Nonslender Delta Wing-Reference-Cited by-同舟云学术

Effect of Passive Bleeding on Flow Structure over a Nonslender Delta Wing

Published:2017-08 Issue:8 Volume:55 Page:2555-2565
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Çelik Alper,Çetin Cenk,Yavuz Mehmet Metin

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055776

Reference45 articles.

1. EarnshawP. B.LawfordJ. A. “Low-Speed Wind Tunnel Experiments on a Series of Sharp-Edged Delta Wings,” Ministry of Aviation Aeronautical Research Council Repts. and Memoranda 3424, London, 1964.

2. Unsteady aerodynamics of nonslender delta wings

3. The discrete vortices from a delta wing

4. WentzW. H. Jr.KohlmanD. L. “Wind Tunnel Investigations of Vortex Breakdown on Slender Sharp-Edged Wings,” NASA CR 98737, 1969.

5. A theory of the flow past a slender delta wing with leading edge separation

Cited by 5 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. Control of Flow Structures on Nonslender Delta Wing Utilizing Nozzle-Type Bleeding Slots;AIAA Journal;2024-09-02

2. Method development for estimation of bleed momentum coefficient using surface pressure measurements and in situ hot wire calibration;Flow Measurement and Instrumentation;2024-07

3. Aerodynamics of non-slender delta and reverse delta wings: Wing thickness, anhedral angle and cropping ratio;Chinese Journal of Aeronautics;2023-04

4. Control of flow structure over a non-slender delta wing using passive bleeding;Aerospace Science and Technology;2020-11

5. Flow Control of Tip/Edge Vortices;AIAA Journal;2018-05