Extending the Leading-Edge Suction Analogy to Nonslender Delta Wings-Reference-Cited by-同舟云学术

Extending the Leading-Edge Suction Analogy to Nonslender Delta Wings

Published:2018-09 Issue:5 Volume:55 Page:2176-2178
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Traub Lance W.¹

Affiliation:

1. Embry-Riddle Aeronautical University, Prescott, Arizona 86301

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034939

Reference21 articles.

1. LambourneN. C.BryerD. W. “The Bursting of Leading-Edge Vortices–Some Observations and Discussion of the Phenomenon,” R&M 3282, ARC, London, England, U.K. April 1961.

2. KegelmanJ. T.RoosF. W. “Effects of Leading-Edge Shape and Vortex Burst on the Flowfield of a 70° Sweep Delta Wing,” AIAA Paper 1989-0086, Jan. 1989. doi:10.2514/6.1989-86

3. Some Experiments with Vortex Breakdown

4. Visualization and wake surveys of vortical flow over a delta wing

5. HummelD. “On the Vortex Formation over a Slender Delta Wing at Large Angles of Incidence,” High Angle of Attack Aerodynamics Conference, AGARD, CP-247, 1979.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. An experimental investigation on the aerodynamic characteristics and vortex dynamics of a flying wing;The Aeronautical Journal;2024-01-08

2. Examination and Prediction of the Lift Components of Low Aspect Ratio Rectangular Flat Plate Wings;Aerospace;2023-06-30

3. Predicting the High-Angle-of-Attack Characteristics of a Delta Wing at Low Speed;Journal of Aircraft;2022-07

4. On Trapeze Wing Aerodynamics Calculations Based on Improved Vortex Lattice Method;DESIGN, CONSTRUCTION, MAINTENANCE;2022-04-13