Add to ORKGResults are presented from static-force tests on biplane wings with large-chord double slotted flaps which turn the slipstream of a single counter rotating propeller downward for vertical take-off. The investigation provided information on the effect of chord length, flap deflection, propeller position, end plates, fuselage, and ground proximity on the efficiency of the wing system in turning the propeller slipstream
Wind tunnel tests of static lateral and directional control of twin-propeller deflected slipstream S...
A small-scale semispan high-lift wing-flap system equipped under the wing with a turboprop engine as...
Longitudinal aerodynamic characteristics of large semispan V/STOL tilt-wing configuration with singl...
Results are presented from static-force tests on biplane wings with large-chord double slotted flaps...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
A unique inverting flap system was investigated on a large scale deflected slipstream model in the A...
The wing employed in this investigation had a 67-percent-chord slotted flap in combination with a 33...
Aerodynamic characteristics of large semispan tilting wing model having double-slotted flap, rotatin...
k An investigation percent-chord sliding percent-chord slat in SUMMARY of the effectiveness of a win...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
Aerodynamic characteristics of large semi-span V/STOL tilt-wing with single propeller tested for mod...
This paper discusses the two major configurations that are usually considered for achieving VTOL whi...
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...
Tests were made of a large-scale tilt-wing deflected-slipstream VTOL airplane with blowing-type BLC ...
Longitudinal aerodynamic characteristics of large scale semispan V/STOL tilt-wing configuration havi...
Wind tunnel tests of static lateral and directional control of twin-propeller deflected slipstream S...
A small-scale semispan high-lift wing-flap system equipped under the wing with a turboprop engine as...
Longitudinal aerodynamic characteristics of large semispan V/STOL tilt-wing configuration with singl...
Results are presented from static-force tests on biplane wings with large-chord double slotted flaps...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
A unique inverting flap system was investigated on a large scale deflected slipstream model in the A...
The wing employed in this investigation had a 67-percent-chord slotted flap in combination with a 33...
Aerodynamic characteristics of large semispan tilting wing model having double-slotted flap, rotatin...
k An investigation percent-chord sliding percent-chord slat in SUMMARY of the effectiveness of a win...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
Aerodynamic characteristics of large semi-span V/STOL tilt-wing with single propeller tested for mod...
This paper discusses the two major configurations that are usually considered for achieving VTOL whi...
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...
Tests were made of a large-scale tilt-wing deflected-slipstream VTOL airplane with blowing-type BLC ...
Longitudinal aerodynamic characteristics of large scale semispan V/STOL tilt-wing configuration havi...
Wind tunnel tests of static lateral and directional control of twin-propeller deflected slipstream S...
A small-scale semispan high-lift wing-flap system equipped under the wing with a turboprop engine as...
Longitudinal aerodynamic characteristics of large semispan V/STOL tilt-wing configuration with singl...