Moment Characteristics of a Low-Aspect Wing in a Finite Flow of Inviscid Fluid,
Abstract
An analysis is made of the change in the position of pressure and aerodynamic centers of a thin plane low-aspect wing moving close to a solid or free surface (in the case of a hydrofoil). The results of this work are based on general relationships of the theory of a thin body and the approximate solutions.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 30, 1973
- Accession Number
- AD0771979
Entities
People
- V. I. Kholyavko
- Yu. F. Usik
Organizations
- National Air and Space Intelligence Center