CHARTS FOR ESTIMATING AERODYNAMIC FORCES ON STOL AIRCRAFT WINGS IMMERSED IN PROPELLER SLIPSTREAMS.
Abstract
Equations and charts are presented for estimating the lift and longitudinal force coefficients of STOL aircraft wings immersed in propeller slipstreams. Sample calculations are made and the results show fair to good correlation with available experimental data. The effect of many design and operating parameters is analyzed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1965
- Accession Number
- AD0634722
Entities
People
- I. Balin
- K. P. Huang
- L. Goland