AN INVESTIGATION OF VTOL OPERATIONAL PROBLEMS DUE TO DOWNWASH EFFECTS
Abstract
Operational problems of VTOL type aircraft caused by downwash effects were investigated utilizing a 3500 horsepower engine and a 15 ft diameter propeller mounted on a 20 ton crane. Results are presented for various propeller disc loadings up to 60 pounds per square foot, for several types of terrain and for various propeller heights and orientation above the terrain. The effects on pilot vision, ground personnel, equipment, aircraft and on aircraft concealment are presented. The effects of downwash were found to be a major operational problem which co ld limit the operational utility of VTOL aircraft.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 12, 1961
- Accession Number
- AD0264560
Entities
People
- R. Pruyn