Numerical Investigation of a Slender Delta Wing with Antisymmetric Leading-Edge Flap Deflection-Reference-Cited by-同舟云学术

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Numerical Investigation of a Slender Delta Wing with Antisymmetric Leading-Edge Flap Deflection

Published:2023-01 Issue:1 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yang Qi¹,Liu Wei²,Chang Xinghua³,Yang Xiaoliang⁴

Affiliation:

1. Ph.D. Student, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410072, China.

2. Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410072, China (corresponding author).

3. Associate Professor, Unmanned Systems Research Center, National Innovation Institute of Defense Technology, Beijing 100071, China.

4. Associate Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410072, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001484

Reference26 articles.

1. Unsteady flow phenomena associated with leading-edge vortices

2. Numerical and experimental investigations of a nonslender delta wing with leading-edge vortex flap

3. Further study on the geometric conservation law for finite volume method on dynamic unstructured mesh

4. Effect of leading-edge flaps on vortices and vortex breakdown

5. Arbitrary Lagrangian-Eulerian Methods

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