METHOD FOR CONTROLLING THE LIMIT LAYER ON THE AERODYNAMIC SURFACE OF A FLYING VEHICLE AND A FLYING VEHICLE.

摘要

A METHOD FOR CONTROLLING THE LIMIT LAYER BY SUCTION OF THE AIR FROM THE SWIRL CHAMBERS PROVIDED IN THE AFT PART OF THE AERODYNAMIC SURFACE OF THE FLYING VEHICLE (FV), WHERE THE SPEED OF THE AIR SUCTION IS REGULATED INCREASING FIRST LIMIT JOINS THE FAIRED SURFACE AND DECREASING BELOW UNTIL THE PRESSURE BEGINS TO FALL ON THE AFT PART OF THE FV. THE PV IS PROVIDED WITH A LIMIT LAYER CONTROL SYSTEM THAT INCLUDES A NUMBER OF TORBELLINO CHAMBERS (1) WHICH ARE HOUSED BY FAIR BODIES (2) AND ARE CONNECTED BY A COMMON CHANNEL (2) THROUGH A RECEIVER (8) FOR A LOW PRESSURE SOURCE (4).