Remarks on Nonlinear Lift and Vortex Separation-Reference-Cited by-同舟云学术

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Remarks on Nonlinear Lift and Vortex Separation

Published:1954-03 Issue:3 Volume:21 Page:212-214
ISSN:1936-9956
Container-title:Journal of the Aeronautical Sciences
language:en
Short-container-title:Journal of the Aeronautical Sciences

Author:

Cheng Hsien K.¹

Affiliation:

1. Aerodynamic Section, Bell Aircraft Corporation, Buffalo, N.Y.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.2971

Reference11 articles.

1. Leading-Edge Separation from Delta Wings at Supersonic Speeds

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1. The leading-edge vortex over a swift-like high-aspect-ratio wing with nonlinear swept-back geometry;Bioinspiration & Biomimetics;2022-10-31

2. A unified theory of slender wings in asymmetric motion, with an application to a swimming sea snake;Journal of Fluid Mechanics;2022-04-12

3. Leading-Edge Vortex as a High-Lift Mechanism for Large-Aspect-Ratio Wings;AIAA Journal;2020-07

4. Aeroelastic interactions and trajectory selection of vortex gusts impinging upon Joukowski airfoils;Journal of Fluids and Structures;2020-07

5. Geometric Nonlinear Control of the Lift Dynamics of a Pitching-Plunging Wing;AIAA Scitech 2020 Forum;2020-01-05

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