The Effect of a Winglet on the Spatial Vortex of a Slender Body at High Angle of Attack,
Abstract
The experimental investigation of the effect of a winglet on the spatial vortex of a slender body at a high angle of attack is presented. This investigation clearly shows that the circulation of the body vortex is minimized by the winglet and the vortex position is lower than that without the winglet, so that the asymmetric problem can be solved.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 07, 1986
- Accession Number
- ADA169925
Entities
People
- Wang Zixing
- Wu Genxing
Organizations
- National Air and Space Intelligence Center