Effects of Plain and Gurney Flaps on a Nonslender Delta Wing

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

Reference40 articles.

1. Experimental Investigation of Influence of Edge Shape on the Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Speeds

2. LambourneN. C.BryerD. W. “The Bursting of Leading-Edge Vortices–Some Observations and Discussion of the Phenomenon,” Aeronautical Research Council RM 3282, London, England, April 1961.

3. HummelD. “On the Vortex Formation over a Slender Delta Wing at Large Angles of Incidence,” High Angle of Attack Aerodynamics, AGARD CP-247, 1979, https://www.sto.nato.int/publications/AGARD.

4. EarnshawP. B.LawfordJ. A. “Low-Speed Wind-Tunnel Experiments on a Series of Sharp-Edged Delta Wings,” Aeronautical Research Council RM 3424, London, England, March 1964.

5. 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.

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