Mechanism modeling and analysis of a small unmanned vehicles using vortex lattice method... For a certain type of small unmanned aerial vehicles (SUAV), using the vortex lattice method (VLM) estimated the aerodynamic derivatives, establishing linear small-perturbation equations based on level and non-sideslipping flight....
Slender body theory programmed for bodies with arbitrary cross section... The program is suitable for determining the angle of attack and sideslipping characteristics of such bodies in the linear range where viscous effects are not predominant....
Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow /A method of computing span loads and the resulting rolling moments for sideslipping wings of arbitrary plan form in incompressible flow is derived....
Flow visualization studies of a sideslipping, canard-configured x-31a-like fighter aircraft model.... The dynamic lag effects, which cause the leeward side vortex to burst earlier thanin the static case during the positive sideslipping motion and later than in the static caseduring the negative sideslipping motion, increase with the magnitude of the sideslipping motion.http://archive.org/details/flowvisualizatio00kimcMajor,...
