The invention relates to aircraft wings in which there is combined therewith a jet propulsion means with thrust augmentation and in which the induced mass flow is derived from airflow over the wing surface including the boundary layer.
Wing and Thrust Augmentor
1971
10 pages
Report
Keine Angabe
Englisch
Thrust augmentor inlet optimization
AIAA | 1986
|Advanced augmentor-wing research
NTRS | 1972
|The Transonic Multifoil Augmentor Wing
AIAA | 1978
|Reversed Cowl Flap Inlet Thrust Augmentor
NTIS | 1975
|Reversed Cowl Flap Inlet Thrust Augmentor
NTIS | 1973
|