A theory of airfoil section past two dimensional nonuniform flow is developed. The theory is based on representation of airfoil section by vortex and source distributions and it can be used for calculation of aircraft wings in homogeneous and inhomogeneous flow, as well as for calculation of straight and radial blade and vane-cascades.
Airfoil Profile in a Nonuniform Flow
1978
53 pages
Report
No indication
English
Airfoil profile in a nonuniform flow
NTRS | 1978
|Thin airfoil in nonuniform parallel streams.
AIAA | 1969
|Thin Airfoil in Nonuniform Parallel Streams
NTIS | 1969
|