Add to ORKGA review of existing publications on wind-tunnel corrections is followed by an approximate method for determining the corrections due to model and wake displacement and to lift. Relations are investigated for fuselages and wings of various spans in closed circular tunnels. A comparison is made between the computations and the tests in the DVL high-speed wind tunnel
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Ailerons having a beveled trailing edge and a blunt-nose overhang of 35 percent aileron chord on an ...
In the vicinity of a body in a wind tunnel the displacement effect of the wake, due to the finite di...
Detailed methods are presented for determining the corrections to results from wind-tunnel tests of ...
Theoretical blockage corrections are presented for a body of revolution and for a three-dimensional ...
A review of existing publications on wind-tunnel corrections is followed by an approximate method fo...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Ailerons having a beveled trailing edge and a blunt-nose overhang of 35 percent aileron chord on an ...
In the vicinity of a body in a wind tunnel the displacement effect of the wake, due to the finite di...
Detailed methods are presented for determining the corrections to results from wind-tunnel tests of ...
Theoretical blockage corrections are presented for a body of revolution and for a three-dimensional ...
A review of existing publications on wind-tunnel corrections is followed by an approximate method fo...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
Ailerons having a beveled trailing edge and a blunt-nose overhang of 35 percent aileron chord on an ...