A Numerical Solution for an Unsteady Two-Dimensional Jet-Flapped Wing.
Abstract
A numerical solution of the two-dimensional jet-flapped airfoil utilizing discrete vortices to represent airfoil and jet vortex distributions is presented for two time-dependent cases. The first concerns an instantaneous deflection of the jet exit angle and the second case involves continuous oscillation of the jet angle. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1972
- Accession Number
- AD0752928
Entities
People
- Glen E. Potter
Organizations
- Pennsylvania State University