Flight Transient Estimation of VTOL Aircraft with Propellers ()
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
No relevant information.