Add to ORKGThe 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record of the aerodynamic characteristics of an airfoil in a wind tunnel. Because of the rapidity of the measurements a complete polar (six components) requires only about three minutes of wind, that is to say, of motive power, which is of interest for wind tunnels with high efficiency factors and may lead to the economical design of large size wind tunnels
This paper is a presentation of the experiments and equipment used in investigations at the Guidonia...
In experimenting with airfoil models in a wind tunnel, the magnitude of the forces acting on the mod...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
Dr. Zahm's report is a description of the six-component wind-tunnel balance in use at the Aerodynami...
The difficulties experienced in properly holding thin tipped or tapered airfoils while testing on an...
The 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record...
Given here is a description of the design of a scientific recording wind tunnel balance. It was deci...
Many experimental arrangements of varying kind involve the problems of assuring a large, steady air ...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
The 6-foot-4-inch wind tunnel and its auxiliary equipment has proven itself capable of continuous an...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
This report describes the layout of the laboratory along with the motor and balance for the wind tun...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
The report contains a description of the DVL wind tunnel. According to the cones fixed, an elliptica...
This paper is a presentation of the experiments and equipment used in investigations at the Guidonia...
In experimenting with airfoil models in a wind tunnel, the magnitude of the forces acting on the mod...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...
Dr. Zahm's report is a description of the six-component wind-tunnel balance in use at the Aerodynami...
The difficulties experienced in properly holding thin tipped or tapered airfoils while testing on an...
The 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record...
Given here is a description of the design of a scientific recording wind tunnel balance. It was deci...
Many experimental arrangements of varying kind involve the problems of assuring a large, steady air ...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
The 6-foot-4-inch wind tunnel and its auxiliary equipment has proven itself capable of continuous an...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
This report describes the layout of the laboratory along with the motor and balance for the wind tun...
An investigation was conducted in the NACA full-scale wind tunnel to determine the aerodynamic chara...
The report contains a description of the DVL wind tunnel. According to the cones fixed, an elliptica...
This paper is a presentation of the experiments and equipment used in investigations at the Guidonia...
In experimenting with airfoil models in a wind tunnel, the magnitude of the forces acting on the mod...
This report contains an exact description of the new wind tunnel of the National Advisory Committee ...