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Full Configuration Drag Estimation of Small-to-Medium Range UAVs and its Impact on Initial Sizing Optimization

  • The paper presents the derivation of a new equivalent skin friction coefficient for estimating the parasitic drag of short-to-medium range fixed-wing unmanned aircraft. The new coefficient is derived from an aerodynamic analysis of ten different unmanned aircraft used on surveillance, reconnaissance, and search and rescue missions. The aircraft are simulated using a validated unsteady Reynolds-averaged Navier Stokes approach. The UAV's parasitic drag is significantly influenced by the presence of miscellaneous components like fixed landing gears or electro-optical sensor turrets. These components are responsible for almost half of an unmanned aircraft's total parasitic drag. The new equivalent skin friction coefficient accounts for these effects and is significantly higher compared to other aircraft categories. It is used to initially size an unmanned aircraft for a typical reconnaissance mission. The improved parasitic drag estimation yields a much heavier unmanned aircraft when compared to the sizing results using available drag data of manned aircraft.

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Metadaten
Author:Falk GöttenORCiD, Felix FingerORCiD, Marc Havermann, Carsten BraunORCiD, Matthew Marino, Cees Bil
DOI:https://doi.org/10.1007/s13272-021-00522-w
ISSN:1869-5590
Parent Title (English):CEAS Aeronautical Journal
Publisher:Springer
Place of publication:Wien
Document Type:Conference Proceeding
Language:English
Year of Completion:2020
Date of the Publication (Server):2020/10/21
Volume:12
First Page:589
Last Page:603
Note:
69. Deutscher Luft- und Raumfahrtkongress 2020, 1. September 2020 - 3. September 2020, online
Link:https://doi.org/10.1007/s13272-021-00522-w
Zugriffsart:campus
Institutes:FH Aachen / Fachbereich Luft- und Raumfahrttechnik
collections:Verlag / Springer