Aerodynamic calculation of unmanned aircraft
MALE UAV design of an increased reliability level
MALE UAV design of an increased reliability level
Formulation of the optimization problem for engine mount design – tractor propeller case
Three surface aircraft (TSA) configuration – flying qualities evaluation
Common computational model for coupling panel method with finite element method
Partially feasible solution space for integrated SATS operations
Stability analysis of the experimental airplane powered by a pulsejet engine
FDM 3D printing method utility assessment in small RC aircraft design
The use of FEA and semi-empirical equations for weight estimation of a passenger aircraft