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ITU Tailless UAV Design

Published: 01 January 2013 Publication History

Abstract

Nowadays, mini Unmanned Aerial Vehicles (UAVs) are utilized in a wide range of reconnaissance and surveillance missions with an ever increasing need for endurance and range. Thus, a slight improvement on these two primary performance parameters is considered as a competitive advantage. In this work, a multi-functional tailless UAV concept and its design process is presented. In comparison to existing conventional UAV designs, the concept is shown to have superior aerodynamic and flight performance characteristics. In addition the detachable wing and body concept provides the much needed flexibility and multi-functionality for using the UAV for a range of operation concepts, in which each concept requires different payloads of distinct weight and size.

References

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NASA X-48B Blended Wing Body Official Page. http:// www.nasa.gov/centers/dryden/research/X-48B (2012). Accessed 19 July 2012.
[2]
Liebeck, R.H., et al.: Blended wing Body Analysis and Design. AIAA (1997).
[3]
Nickel, K., Wolfahrt, M.: Tailless Aircraft in Theory and Practice. AIAA Education Series (1994).
[4]
Kroo, I., Watayama, S.: The Challenge and Promise of Blended-wing-body Optimization. AIAA (1998).
[5]
Raymer, D.P.: Aircraft Design: A Conceptual Approach, 2nd edn. AIAA Education Series (1992).
[6]
Viieru, D., Albertani, R., Shyy, W., Ifju, P.: Effect of tip vortex on wing aerodynamics of micro aerial vehicles. In: 22th AIAA Conference Paper, Reno (2004).
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CD-Adapco: Instruction Manual of Star CCM+6.04.011 (2011).

Cited By

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  • (2022)Co-design Optimization of a Novel Multi-identity Drone Helicopter (MICOPTER)Journal of Intelligent and Robotic Systems10.1007/s10846-022-01755-5106:3Online publication date: 1-Nov-2022
  • (2018)Design of a Commercial Hybrid VTOL UAV SystemJournal of Intelligent and Robotic Systems10.1007/s10846-013-9900-074:1-2(371-393)Online publication date: 30-Dec-2018
  • (2016)Rapid Prototyping of a Fixed-Wing VTOL UAV for Design TestingJournal of Intelligent and Robotic Systems10.1007/s10846-015-0328-684:1-4(639-664)Online publication date: 1-Dec-2016

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Information & Contributors

Information

Published In

cover image Journal of Intelligent and Robotic Systems
Journal of Intelligent and Robotic Systems  Volume 69, Issue 1-4
January 2013
492 pages

Publisher

Kluwer Academic Publishers

United States

Publication History

Published: 01 January 2013

Author Tags

  1. Flying wing aircraft
  2. Tailless aircraft
  3. UAV design and development
  4. Unmanned aerial vehicles

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Cited By

View all
  • (2022)Co-design Optimization of a Novel Multi-identity Drone Helicopter (MICOPTER)Journal of Intelligent and Robotic Systems10.1007/s10846-022-01755-5106:3Online publication date: 1-Nov-2022
  • (2018)Design of a Commercial Hybrid VTOL UAV SystemJournal of Intelligent and Robotic Systems10.1007/s10846-013-9900-074:1-2(371-393)Online publication date: 30-Dec-2018
  • (2016)Rapid Prototyping of a Fixed-Wing VTOL UAV for Design TestingJournal of Intelligent and Robotic Systems10.1007/s10846-015-0328-684:1-4(639-664)Online publication date: 1-Dec-2016

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