Experimental Exploration of Bioinspired Planar Wingtip Devices for a Flat-Plate Wing in the Low Reynolds Number Regime

Author:

Borah Bastav1,Verma Anand2ORCID,Kulkarni Vinayak3ORCID,Saha Ujjwal K.4ORCID

Affiliation:

1. Ph.D. Student, Dept. of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati, Assam 781039, India.

2. Ph.D. Student, Dept. of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati, Assam 781039, India. ORCID: .

3. Professor, Dept. of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati, Assam 781039, India (corresponding author). ORCID: .

4. Professor, Dept. of Mechanical Engineering, Indian Institute of Technology Guwahati, Guwahati, Assam 781039, India. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Reference48 articles.

1. Ailinger K. 1997. “Micro air vehicle (MAV) development at NRL.” In Proc. Association of Unmanned Vehicle Systems Int. Conf. AUVSI’97. Arlington VA: Association of Unmanned Vehicle Systems.

2. Albertani R. 2005. “Experimental aerodynamics of elastic deformation characterisation of low aspect ratio finite wings applied to micro air vehicles.” Ph.D. thesis Dept. of Mechanical and Aerospace Engineering Univ. of Florida Gainesville.

3. Aerodynamic Coefficients and Deformation Measurements on Flexible Micro Air Vehicle Wings

4. Ananda G. K. P. P. Sukumar and M. S. Selig. 2012. “Low-to-moderate aspect ratio wings tested at low Reynolds numbers.” In Proc. 30th AIAA Applied Aerodynamics Conf. New Orleans LA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2012-3026.

5. Measured aerodynamic characteristics of wings at low Reynolds numbers

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