English (United Kingdom)

https://curated-unify.zendy.io/wp-json/zendy-region/v1/featured_content/oa?rat=en

https://curated-unify.zendy.io/wp-json/zendy-region/v1/highlighted_journal/

Global: Zendy Plus annual

Presents the access of premium content as premium feature

Premium Content

Presents the keyphrase highlighting as premium feature

Keyphrase Highlighting

Presents the summarisation as premium feature

Summarisation

Insights

Presents the pdf analysis as premium feature

PDF Analysis

Presents the zaia usage as premium feature

ZAIA

Global: Zendy Plus monthly

Global: Zendy Tools annual

Global: Zendy Tools monthly

Global: Zendy Free Plan

For the development of an unmanned aerial vehicle (UAV) simulator, an aerodynamic analysis was performed. To analyze the aerodynamic coefficient, an unsteady numerical method (time-domain panel method) was used. This panel method was based on the Dirichlet boundary condition coupled with a time-stepping method. The FreeWake method was also used to get more accurate results. The proposed numerical method was validated by comparing our results with experimental data. Through the aerodynamic analysis, longitudinal, lateral, directional and dynamic derivatives were obtained. To build the database for the UAV, the results were predicted rationally. This research will contribute to designing UAVs as well as to developing UAV simulators.

Study on the Extraction of Aerodynamic Coefficients for the Development of an UAV Simulator using the Unsteady Time-Domain Panel Method