Experimental study on the effects of wing sweep on Gurney flap performance-Reference-Cited by-同舟云学术

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Experimental study on the effects of wing sweep on Gurney flap performance

Published:2016-08 Issue: Volume:55 Page:57-63
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Traub Lance W.,Chandrashekar Samarth M.

Funder

Embry Riddle Aeronautical University

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. Aerodynamic Design of Aircraft;Kuchemann,1978

2. Fundamentals of Aerodynamics;Anderson,2001

3. Aerodynamic lift at supersonic speeds;Busemann,1935

4. Fluid Dynamic Lift;Hoerner,1975

5. An investigation of the pressure distributions on a 45 degree swept half wing including the effects of upper surface spoilers;Dobson,1971

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1. The flow control mechanism of trailing-edge Gurney flap on a 50°-swept delta wing in forced pitching;Physics of Fluids;2024-08-01

2. Aerodynamic performance and wake development of NACA 0018 airfoil with serrated gurney flaps;Frontiers in Energy Research;2024-05-03

3. Aerodynamic Enhancement of Vertical-Axis Wind Turbines Using Plain and Serrated Gurney Flaps;Applied Sciences;2023-11-24

4. Sweep and Thickness Effects on Flat-Plate Wings at Low Reynolds Number;Journal of Aircraft;2021-11

5. Effect of Gurney Flap on Performance and Aeroacoustics of Variable-Pitch Axial Fans;AIAA Journal;2020-06

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