A brief outline of augmentor wing research is presented and is followed by a discussion of large scale wind tunnel test results for a swept augmentor wing configuration. The results show that the augmentor wing can be applied to high speed swept wing designs with little adverse effect on either the basic performance of the augmentor or the longitudinal characteristics, including maximum lift and stall. Three lateral control devices were shown to be effective and ground effect was measured for several complete aircraft configurations. (Author)
Aerodynamic Characteristics of a Swept Augmentor Wing
1972
24 pages
Report
Keine Angabe
Englisch
Aerodynamic characteristics of a swept augmentor wing
NTRS | 1972
|Aerodynamic characteristics of a swept augmentor wing
NTRS | 1972
|Advanced augmentor-wing research
NTRS | 1972
|NTIS | 1971
|The Transonic Multifoil Augmentor Wing
AIAA | 1978
|