Add to ORKGAn investigation of the longitudinal and lateral stability and control and Performance characteristics of a six-propeller deflected- slipstream vertical-take-off-and-landing (VTOL) model in the transition speed range was conducted in the 17-foot test section of the Langley 300-MPH 7- by 10-foot tunnel. A complete analysis of the data was not conducted. A modest amount of blowing boundary-layer control was necessary to achieve transition without wing stall
Wind tunnel tests of stability and control characteristics of large scale model representative of pr...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
"An investigation of the aerodynamic characteristics of a powered semispan tilting-shrouded-propelle...
Results are presented of a wind-tunnel investigation of the longitudinal stability, control, and per...
Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...
Longitudinal stability and control characteristics of powered model of twin-propeller deflected-slip...
Ground proximity effects on longitudinal, lateral, and control aerodynamic characteristics of tilt w...
Wind tunnel tests of static lateral and directional control of twin-propeller deflected slipstream S...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
Wind tunnel study of lateral and directional aerodynamic characteristics of powered four-duct propel...
The wing employed in this investigation had a 67-percent-chord slotted flap in combination with a 33...
This paper discusses the two major configurations that are usually considered for achieving VTOL whi...
A study is presented of the improvements in take-off and landing distances possible with a conventio...
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...
Wind tunnel tests of stability and control characteristics of large scale model representative of pr...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
"An investigation of the aerodynamic characteristics of a powered semispan tilting-shrouded-propelle...
Results are presented of a wind-tunnel investigation of the longitudinal stability, control, and per...
Results are presented of a wind-tunnel investigation of the aerodynamic stability, control, and perf...
Longitudinal stability and control characteristics of powered model of twin-propeller deflected-slip...
Ground proximity effects on longitudinal, lateral, and control aerodynamic characteristics of tilt w...
Wind tunnel tests of static lateral and directional control of twin-propeller deflected slipstream S...
An investigation was conducted in order to determine the effectiveness of blowing a jet of air over ...
Propeller slipstream effects as determined from wing pressure distribution of a large-scale six-prop...
Wind tunnel study of lateral and directional aerodynamic characteristics of powered four-duct propel...
The wing employed in this investigation had a 67-percent-chord slotted flap in combination with a 33...
This paper discusses the two major configurations that are usually considered for achieving VTOL whi...
A study is presented of the improvements in take-off and landing distances possible with a conventio...
The model was tested at two different elevations with the wing pivot at 1.008 and 2.425 propeller di...
Wind tunnel tests of stability and control characteristics of large scale model representative of pr...
Report presents the results of a study of data obtained in the NACA full-scale wind tunnel concernin...
"An investigation of the aerodynamic characteristics of a powered semispan tilting-shrouded-propelle...