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Kumar, V., Sharma, R., Sharma, S., Chandel, S. and Kumar, S. (2021) A Review on Design Methods of Vertical Take-Off and Landing UAV Aircraft. In: Proceedings of International Conference on Materials Science and Engineering, Mathura, 18th-19th December 2020, Article No. 012142.
https://www.researchgate.net/publication/351892893_A_Review_on_Design_Methods_of_Vertical_take-off_and_landing_UAV_aircraft

has been cited by the following article:

• TITLE: Flight Transient Estimation of VTOL Aircraft with Propellers

  AUTHORS: Nickolay Zosimovych

  KEYWORDS: Vertical Take-Off and Landing (VTOL) Drone, Propeller, Transient, Thrust, Vector, Modeling, Kinematic, Aerodynamic Coefficient

  JOURNAL NAME: Advances in Aerospace Science and Technology, Vol.7 No.1, March 30, 2022

  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.