Leading-Edge Vortex as a High-Lift Mechanism for Large-Aspect-Ratio Wings-Reference-Cited by-同舟云学术

Leading-Edge Vortex as a High-Lift Mechanism for Large-Aspect-Ratio Wings

Published:2020-07 Issue:7 Volume:58 Page:2806-2819
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Ben-Gida Hadar¹,Gurka Roi²,Weihs Daniel¹

Affiliation:

1. Technion—Israel Institute of Technology, 32000 Haifa, Israel

2. Coastal Carolina University, Conway, South Carolina 29528

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference69 articles.

1. WinterH. “Flow Phenomena on Plates and Airfoils of Short Span,” NACA T&M 798, 1936.

2. WilsonH. A. Jr.LovellC. J. “Full-Scale Investigation of the Maximum Lift and Flow Characteristics of an Airplane Having Approximately Triangular Plan Form,” NACA R&M L6K20, 1947.

3. Remarks on Nonlinear Lift and Vortex Separation

4. Effect of Leading-Edge Separation on the Lift of a Delta Wing

5. PolhamusE. C. “A Concept of the Vortex Lift of Sharp-Edge Delta Wings Based on a Leading-Edge-Suction Analogy,” NASA TN D-3767, 1966.

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