Experimental Investigation of Effect of Winglets on the Aerodynamic Performance of a Mini UAV-Reference-Cited by-同舟云学术

Experimental Investigation of Effect of Winglets on the Aerodynamic Performance of a Mini UAV

Published:2021-01 Issue:1 Volume:34 Page:04020089
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Deshpande Parag¹^ORCID,Vikraman Akhil²,Anand Shashant³,Antony Roshan⁴,Dodamani Ravi⁵,C. S. Suraj⁴,Ajith Kumar R.⁶

Affiliation:

1. Senior Scientist, CSIR-National Aerospace Laboratories, UAV Design and Integration Division, Bangalore 560017, India (corresponding author). ORCID: .

2. Post-Graduate Student, Dept. of Mechanical Engineering, Amrita Vishwa Vidyapeetham, Amritapuri Campus, Kollam 690546, India.

3. Scientist, CSIR-National Aerospace Laboratories, UAV Design and Integration Division, Bangalore 560017, India.

4. Principal Scientist, CSIR-National Aerospace Laboratories, UAV Design and Integration Division, Bangalore 560017, India.

5. Senior Scientist, CSIR-National Aerospace Laboratories, UAV Design and Integration Division, Bangalore 560017, India.

6. Professor, Dept. of Mechanical Engineering, Amrita Vishwa Vidyapeetham, Amritapuri Campus, Kollam 690546, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001206

Reference20 articles.

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2. AeroVironment. n.d. “Raven b UAV.” Accessed June 16 2020. https://www.avinc.com/tuas/raven.

3. Air Force Technology. 2011. “BirdEye 400 unmanned aerial vehicle.” Accessed June 16 2020. https://www.airforce-technology.com/projects/birdeye400/.

4. Army Technology. 2005. “EMT Aladin unmanned aerial vehicle.” Accessed June 16 2020. https://www.army-technology.com/projects/emt-aladin-uav/.

5. AviaPro. 2007. “Zala aero zala 421-12.” Accessed June 16 2020. https://avia-pro.net/blog/zala-aero-zala-421-12.

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