Effect of Thickness-to-Chord Ratio on Flow Structure of a Low Swept Delta Wing-Reference-Cited by-同舟云学术

Effect of Thickness-to-Chord Ratio on Flow Structure of a Low Swept Delta Wing

Published:2018-12 Issue:12 Volume:56 Page:4657-4668
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Gülsaçan Burak¹,Şencan Gizem¹,Yavuz Mehmet Metin¹

Affiliation:

1. Middle East Technical University, 06800 Ankara, Turkey

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057083

Reference21 articles.

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

2. Unsteady aerodynamics of nonslender delta wings

3. Unsteady flow phenomena associated with leading-edge vortices

4. WitcofskiR. D.MarcumD. C. Jr. “Effect of Thickness and Sweep Angle on the Longitudinal Aerodynamic Characteristics of Slab Delta Planforms at a Mach Number of 20,” NASA TN-D 3459, June 1966.

5. Effects of leading-edge bevel angle on the aerodynamic forces of a non-slender 50° delta wing

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