Add to ORKGTests were made of a large-scale tilt-wing deflected-slipstream VTOL airplane with blowing-type BLC trailing-edge flaps. The model was tested with flap deflections of 0 deg. without BLC, 50 deg. with and without BLC, and 80 deg. with BLC for wing-tilt angles of 0, 30, and 50 deg. Included are results of tests of the model equipped with a leading-edge flap and the results of tests of the model in the presence of a ground plane
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
A wind-tunnel investigation was made to determine the effects of ejecting high-velocity air near the...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
Wind tunnel test of ground effect of 35-deg swept- back wing jet transport equipped with boundary la...
A study is presented of the improvements in take-off and landing distances possible with a conventio...
Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/...
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...
The investigation was conducted to determine the static stability and control characteristics of the...
A unique inverting flap system was investigated on a large scale deflected slipstream model in the A...
Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Results are presented of a wind-tunnel investigation of the longitudinal stability, control, and per...
An investigation of the stability and control of a high-wing transport vertical-take-off airplane wi...
Tests in the Ames 40- by 80-foot wind tunnel of the static longitudinal characteristics of the Repub...
The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail ...
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
A wind-tunnel investigation was made to determine the effects of ejecting high-velocity air near the...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
Wind tunnel test of ground effect of 35-deg swept- back wing jet transport equipped with boundary la...
A study is presented of the improvements in take-off and landing distances possible with a conventio...
Wind tunnel tests of wing stall, performance, and longitudinal stability & control of large model v/...
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...
The investigation was conducted to determine the static stability and control characteristics of the...
A unique inverting flap system was investigated on a large scale deflected slipstream model in the A...
Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...
Tests were made on a model wing with three different sized split trailing-edged flaps, in the NACA 7...
Results are presented of a wind-tunnel investigation of the longitudinal stability, control, and per...
An investigation of the stability and control of a high-wing transport vertical-take-off airplane wi...
Tests in the Ames 40- by 80-foot wind tunnel of the static longitudinal characteristics of the Repub...
The aerodynamic characteristics of a full scale executive type jet transport aircraft with a T-tail ...
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
A wind-tunnel investigation was made to determine the effects of ejecting high-velocity air near the...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
