Aerodynamic Numerical Analysis of the Low Reynolds Number Diamond Joined-Wing Configuration Unmanned Aerial Vehicle-Reference-Cited by-同舟云学术

Aerodynamic Numerical Analysis of the Low Reynolds Number Diamond Joined-Wing Configuration Unmanned Aerial Vehicle

Published:2018-08-21 Issue:3 Volume:19 Page:544-562
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Sun Junlei,Wang Heping,Zhou Zhou,Lei Shan

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

http://link.springer.com/article/10.1007/s42405-018-0072-9/fulltext.html

Reference23 articles.

1. The Wolkovitch J, Wing Joined (1982) An overview. J Aircraft 23(3):161–178

2. Kroo I, Smith S, Gallman J (1991) Aerodynamic and structural studies of joined-wing aircraft. J Aircraft 28(1):74–81

3. Craft RL (2005) Drag Estimates for the joined-wing sensor craft, 05J02. Airforce Inst of Tech Wright-patterson Afb Oh School of Engineering And Management, Ohio:AFIT, pp 131-139

4. Pérez-álvarez J, Cuerno-Rejado C, Meseguer J (2015) Aerodynamic parametric analysis of an unconventional joined-wing aircraft configuration[J]. Proc Inst Mech Eng, Part G 230:1–17

5. Bond V, Canfield RA, Matos M, et al. (2007) Wind tunnel testing of a twisted wing for longitudinal control in a joined-wing aircraft//48th structures structural dynamics and materials conference, Honolulu:AIAA. 1772, pp 1–7

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