Typical 4-engine jet has wing of aspect ratio 7; 3-component longitudinal force and moment data and boundary layer flow requirements are presented and results analyzed in terms of estimated take-off and landing performance; effect on performance of source of boundary-layer-control airflow is considered.
Large-scale wind-tunnel tests and evaluation of low-speed performance of 35° sweptback wing jet transport model equipped with blowing boundary-layer-control flap and leading-edge slat
NASA -- Tech Note
1960
52 pages
Report
Englisch
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