Effect of Anhedral–Dihedral Angles on 76-40° Double-Delta Wing at Low Speeds-Reference-Cited by-同舟云学术

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Effect of Anhedral–Dihedral Angles on 76-40° Double-Delta Wing at Low Speeds

Published:2019-11 Issue:6 Volume:32 Page:04019091
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Roy D.¹,Kumar Priyank²^ORCID,Das Sudip³

Affiliation:

1. PG Student, Dept. of Space Engineering and Rocketry, Birla Institute of Technology, Mesra, Ranchi, Jharkhand 835215, India.

2. Assistant Professor, Dept. of Space Engineering and Rocketry, Birla Institute of Technology, Mesra, Ranchi, Jharkhand 835215, India (corresponding author). ORCID: .

3. Professor, Dept. of Space Engineering and Rocketry, Birla Institute of Technology, Mesra, Ranchi, Jharkhand 835215, India.

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.1943-5525.0001079

Reference25 articles.

1. Experimental and Numerical Investigation of 65 Degree Delta and 65/40 Degree Double-Delta Wings

2. Some aerodynamic principles for the design of swept wings

3. Numerical investigation of high incidence flow over a double-delta wing

4. Vortex interaction and breakdown over double-delta wings

5. Review of flow control mechanisms of leading-edge vortices

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