An experimental investigation on tapered wings with leading-edge protuberances

Particle Image Velocimetry (PIV) experiments were conducted in a water tunnel to study vortex interactions around tapered swept wings with leading edge tubercles. Two airfoil models based on the SD7032 airfoil profile were tested at Reynolds number 9100 and angles of attack (α) of -10°,10° and 25°,...

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Bibliographic Details
Main Author: Ee, Marcus Joon Leng
Other Authors: New Tze How, Daniel
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2023
Subjects:
Online Access:https://hdl.handle.net/10356/168370
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Institution: Nanyang Technological University
Language: English