Experimental Investigation of the Effect of Trailing-Edge Flaps on Delta Wings-Reference-Cited by-同舟云学术

Experimental Investigation of the Effect of Trailing-Edge Flaps on Delta Wings

Published:2017-09 Issue:5 Volume:54 Page:1945-1959
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.C034273

Reference44 articles.

1. LegendreR. “Flow in the Neighborhood of the Apex of a Highly Swept Wing at Moderate Incidences,” Aeronautical Research Council Rept. 16, London, 1954.

2. BrownC. E.MichaelW. H. Jr. “On Slender Delta Wings with Leading Edge Separation,” NASA TN 3430, 1955.

3. A theory of the flow past a slender delta wing with leading edge separation

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

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

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