Title Stačiakampio sparno aerodinaminių charakteristikų tyrimas /
Translation of Title Research of aerodynamics characterictics of rectangular wing.
Authors Gascevičius, Elanas
Full Text Download
Pages 63
Keywords [eng] Wing ; plane ; fuselage
Abstract [eng] This master's thesis studied the finite rectangular wing lift coefficient by using the Karl - Heinz Horstmann program, known as discrete vortex method. This paper examined the theoretical calculations of lift at different angles of attack. This study shows that this method is very good to calculate the lift coefficients and the induction drag values.
Type Master thesis
Language Lithuanian
Publication date 2012