Experimental Investigation of Incompressible Flow Past Jet Flapped Airfoils.
Abstract
Experiments were conducted in low-speed wind tunnel to investigate the aerodynamic characteristics of an airfoil with a jet flap deflected at ninety degrees, in and out of ground effect. These tests consisted of detailed static pressure measurements on the airfoil, and helium bubble flow visualization studies of the resulting flow patterns. Substantial agreement was obtained with previous experiments conducted in England. (Modified author abstract)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1974
- Accession Number
- AD0778631
Entities
People
- Carl Mark Tankersley
Organizations
- Naval Postgraduate School