Verifying the Effect of Wingtip Propellers on Drag Through In-Flight Measurements
Author:
Affiliation:
1. University of Stuttgart, 70569 Stuttgart, Germany
Funder
German Federal Aeronautical Research Programme
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C036490
Reference19 articles.
1. Effects of wingtip-mounted propellers on wing lift and induced drag.
2. PattersonJ. C. Jr.FlechnerS. G. “Explanatory Wind-Tunnel Investigation of a Wingtip-Mounted Vortex Turbine for Vortex Energy Recovery,” NASA TP 2468, 1985.
3. Wingtip-Mounted Propellers: Aerodynamic Analysis of Interaction Effects and Comparison with Conventional Layout
4. SobronA. “On Subscale Flight Testing: Applications in Aircraft Conceptual Design,” Ph.D. Thesis, Division of Fluid and Mechatronic Systems, Linköping Univ., Linköping, Sweden, 2018. 10.3384/lic.diva-152488
5. Methods For Drag Determination In Flight
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