Induced Velocities of Free Wing Vortices with a Curved Axis in a Plane,
Abstract
The report calculates induced velocities of a wing with a curved axis not perpendicular to the velocity of the incoming flow. The velocity produced at each point of the surrounding space by the wing vortex system will consist of two parts: the velocity created by the vortex sheet and the velocity created by the lifting vortex line. The calculation of the velocity created by the wing vortices is the content of this article. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 04, 1972
- Accession Number
- AD0749843
Entities
People
- K. I. Kondrat
Organizations
- National Air and Space Intelligence Center