Advances in Aerospace Science and Technology

Volume 7, Issue 1 (March 2022)

ISSN Print: 2473-6708   ISSN Online: 2473-6724

Google-based Impact Factor: 0.59  Citations  

Flight Transient Estimation of VTOL Aircraft with Propellers

HTML  XML Download Download as PDF (Size: 1612KB)  PP. 85-95  
DOI: 10.4236/aast.2022.71005    298 Downloads   1,443 Views  Citations

ABSTRACT

Methodological issues associated with the determination of the vertical take-off and landing aerodynamic parameters equipped with two rotary propellers during take-off and hovering, descent and landing are studied in the proposed article. During the computer simulation process, kinematics parameters diagrams were made, aerodynamic coefficients and propellers thrust components at all stages of aircraft take-off were estimated. That numerical data can be used in a preliminary stage of aerodynamic design for the vertical take-off and landing aircraft and electric drones at the determination of control and equalization elements geometric and kinematic parameters.

Share and Cite:

Zosimovych, N. (2022) Flight Transient Estimation of VTOL Aircraft with Propellers. Advances in Aerospace Science and Technology, 7, 85-95. doi: 10.4236/aast.2022.71005.

Cited by

[1] Hex-rotor aircraft dynamics and simulation
AIP Conference Proceedings, 2023
[2] Design and Development of Vertical Take-Off and Landing (VTOL) Drone for Surveillance
International Journal of …, 2023

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