Post Stall Control of Swept Wings,
Abstract
The work conducted on this effort is described in detail in six papers which were presented at various meetings. Copies of the papers are attached to this report. A brief description of this material is provided below. At the beginning of this effort, the fundamental character of the flow was investigated. In the first publication generated, we discuss the transient flow field over a delta wing during pitch-up motions to very large angles of attack. Emphasis was directed at the growth and the eventual breakdown of leading edge vortices.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1995
- Accession Number
- ADA299820
Entities
People
- Demetri Telionis
Organizations
- Virginia Tech