Effect of Yaw Angles on Aerodynamics of a Slender Delta Wing-Reference-Cited by-同舟云学术

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Effect of Yaw Angles on Aerodynamics of a Slender Delta Wing

Published:2019-09 Issue:5 Volume:32 Page:04019074
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Karasu Ilyas¹,Sahin Besir²,Tasci M. Oguz³,Akilli Huseyin⁴

Affiliation:

1. Assistant Professor, Dept. of Aerospace Engineering, Adana Alparslan Turkes Science and Technology Univ., Adana BTU Havacılık Mühendisliği, Gultepe Mah., Sarıcam, Adana PK 01250, Turkey.

2. Professor, Dept. of Mechanical Engineering, Head of Energy Division, Cukurova Univ., Makine Mühendisliği, Sarıcam, Adana PK 01330, Turkey (corresponding author).

3. Ph.D. Student, Dept. of Mechanical Engineering, Cukurova Univ., Makine Mühendisliği, Sarıcam, Adana PK 01330, Turkey.

4. Professor, Dept. of Mechanical Engineering, Cukurova Univ., Makine Mühendisliği, Sarıcam, Adana PK 01330, Turkey.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001066

Reference34 articles.

1. Unsteady flow phenomena associated with leading-edge vortices

2. Dye Visualization of the Flow Structure over a Yawed Nonslender Delta Wing

3. Observation of the Vortical Flow over a Yawed Delta Wing

4. Vortex structures for flow over a delta wing with sinusoidal leading edge

5. Aspects of vortex breakdown

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2. Experimental investigation of dynamic ground boundary condition for a non-slender delta wing;CEAS Aeronautical Journal;2024-05-30

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

4. Effect of ground on aerodynamics and longitudinal static stability of a non-slender delta wing;Aerospace Science and Technology;2022-11

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