Design and development of an Air Supply Unit for Circulation Control Wing-based UAVs-Reference-Cited by-同舟云学术

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Design and development of an Air Supply Unit for Circulation Control Wing-based UAVs

Published:2015-03 Issue: Volume: Page:
ISSN:
Container-title:2015 IEEE Aerospace Conference
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Author:

Kanistras Konstantinos,Saka Pranith Chander,Valavanis Kimon P.,Vitzilaios Nikolaos I.,Rutherford Matthew J.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/7114093/7118873/07119204.pdf?arnumber=7119204

Cited by 4 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. Experimental Study on Aerodynamic Properties of Circulation Control Airfoil with Plasma Jet;Lecture Notes in Electrical Engineering;2019

2. System Identification and Controller Implementation of a Centrifugal Compressor for Circulation Control Applications;Journal of Intelligent & Robotic Systems;2018-01-23

3. Design and Development of a Control Scheme for the UC2AV: Unmanned Circulation Control Aerial Vehicle;55th AIAA Aerospace Sciences Meeting;2017-01-05

4. Low Speed Wind Tunnel Investigation of a Circulation Control Wing for Enhanced Lift;33rd AIAA Applied Aerodynamics Conference;2015-06-19

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