An Experimental Investigation of the Effect of a Fuselage on Wing Characteristics.
Abstract
A series of experimental investigations utilizing flow visualization, force measurement and pressure distribution techniques to investigate the effect on wing lift of fuselage placement and cross-sectional shape are reported. Emphasis is placed on conditions involving large circulation including the use of circulation control.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1975
- Accession Number
- ADA003955
Entities
People
- Fumio Yoshino
Organizations
- Princeton University