TY  - JOUR
AB  - 3. In a wing, associated with a relative flow of fluid; a means to interpose, between a wing and its boundary layer, a stream of fluid of energy content substantially as large as that of the relative flow, comprising a wing body possessing in its upper surface a spanwise slot extending at least along a major portion of the semi‐span, a divided upper surface to the rear of the said slot to form a second slot and an induction opening leading into the wing, a conduit to connect the induction opening and the forward slot, and a fluid conveying conduit to provide a rearward flow through the exit of the second slot.
VL  - 8
IS  - 8
SN  - 0002-2667
DO  - 10.1108/eb030087
UR  - https://doi.org/10.1108/eb030087
PY  - 1936
Y1  - 1936/01/01
TI  - U.S. Patent Specifications
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 236
EP  - 236
Y2  - 2024/04/23
ER  -