In-flight drag measurement and validation for a medium-sized UAV

Julius Bartasevicius, Mirko Hornung

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Scopus citations

Abstract

In order to maintain low cruise speeds and high efficiency for unmanned aerial vehicles, low wing loading designs are required. Consequently, the influence of atmospheric turbulence on aerodynamic measurements performed on such vehicles increases, especially on drag. The current study evaluates if it is possible to measure the drag of such medium-sized UAVs in-flight. For this reason, a 7m wingspan, 65kg take-off mass conventional configuration UAV is used. Global, induced as well as component drag (airbrakes, landing gear and flaps) is extracted using the data recorded in-flight with high atmospheric turbulence. The measurements are compared to CFD studies as well as empirical data for the airbrakes.

Original languageEnglish
Title of host publicationAIAA SciTech Forum and Exposition, 2023
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106996
DOIs
StatePublished - 2023
EventAIAA SciTech Forum and Exposition, 2023 - Orlando, United States
Duration: 23 Jan 202327 Jan 2023

Publication series

NameAIAA SciTech Forum and Exposition, 2023

Conference

ConferenceAIAA SciTech Forum and Exposition, 2023
Country/TerritoryUnited States
CityOrlando
Period23/01/2327/01/23

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