Drag Reduction Effect of a Variable Camber Wing of a Transport Aircraft Based on Trailing Edge Flap Deflection of Small Angles-Reference-Cited by-同舟云学术

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Drag Reduction Effect of a Variable Camber Wing of a Transport Aircraft Based on Trailing Edge Flap Deflection of Small Angles

Published:2019 Issue: Volume: Page:1508-1514
ISSN:1876-1100
Container-title:Lecture Notes in Electrical Engineering
language:
Short-container-title:

Author:

Liu Yi,Ouyang Shaoxiu,Zhao Xiaoxia

Publisher

Springer Singapore

Link

http://link.springer.com/content/pdf/10.1007/978-981-13-3305-7_120

Reference10 articles.

1. Boeing (1980) Assessment of variable camber for application to transport aircraft. NASA-CR-158930

2. Bolonkin A, Gilyard GB (1999) Estimated benefits of variable-geometry wing camber control for transport aircraft. NASA-TM-1999-206586

3. Boltz FW, Pena DF (1977) Aerodynamic characteristics of an F-8 aircraft configuration with a variable camber wing at Mach numbers from 0.70 to 1.15. NASA-TM-78432

4. Committee of Aircraft Design Manual (2002) Aircraft design manual volume 6 aerodynamic design. Aviation Industry Press, Beijing (in Chinese)

5. Ferris JC (1977) Wind-tunnel investigation of a variable camber and twist wing. NASA-TN-D-8475

Cited by 2 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. Methodology for Evaluating a Distributed Variable-Camber Trailing-Edge System in Preliminary Aircraft Design;Journal of Aircraft;2024-07

2. Design and analysis of variable camber wing of propeller aircraft using the actuator disc method;The Aeronautical Journal;2022-03-24

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