Results of investigation designed to study how pilots use high lift available with blowing boundary-layer-control leading- and trailing-edge flaps to provide operation experience, and to determine limiting factors in choice of landing approach speed when wing stall is delayed to high angles of attack.
Flight investigation of low-speed characteristics of 45° swept-wing fighter-type airplane with blowing boundary-layer control applied to leading- and trailing-edge flaps
NASA -- Tech Note
1960
44 pages
Report
Englisch
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