AERODYNAMIC ANALYSIS OF WING WITH LEADING EDGE PROTUBERANCES USING PRANDTL'S LIFTING LINE THEORY
Author:
Publisher
Begell House
Subject
General Medicine
Link
https://www.dl.begellhouse.com/download/article/1d3f33261e09b38b/FMR4904(3)-43017.pdf
Reference36 articles.
1. Numerical Lifting Line Theory Applied to Drooped Leading Edge Wings below and above Stall;Anderson J.D.;J. Aircraft,1980
2. Statistical-Empirical Modeling of Airfoil Noise Subjected to Leading-Edge Serrations;Biedermann T.M.;AIAA J,2017
3. The Effects of Tubercles on Swept Wing Performance at Low Angles of Attack;Bolzon M.D.,2014
4. Parametric Study of the Effects of a Tubercle's Geometry on Wing Performance through the Use of the Lifting Line Theory;Bolzon M.D.,2016
5. Force Measurements and Wake Surveys of a Swept Tubercled Wing;Bolzon M.D.;J. Aerosp. Eng,2017
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