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
An improved method of calibrating a wind-tunnel force balance involves the use of a unique load appl...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-s...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
The 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record...
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...
A flow-through balance is provided which includes a non-metric portion and a metric portion which fo...
A new six axis air balance was delivered to the NASA Glenn Research Center. This air balance has an ...
Research on wingsuit aerodynamics requires specialized wind tunnel equipment. There is the potential...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
A discussion on the fundamental concepts associated with wind tunnel forces measurement systems (bal...
A typical educational wind tunnel need only measure the lift and drag forces and be able to control ...
M.Phil.In today's world with its competitive environment there is a need to shorten product developm...
Brief details of gauging work carried out on the\ud single component drag balance is discussed. The ...
An improved method of calibrating a wind-tunnel force balance involves the use of a unique load appl...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-s...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
The 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record...
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...
A flow-through balance is provided which includes a non-metric portion and a metric portion which fo...
A new six axis air balance was delivered to the NASA Glenn Research Center. This air balance has an ...
Research on wingsuit aerodynamics requires specialized wind tunnel equipment. There is the potential...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
A discussion on the fundamental concepts associated with wind tunnel forces measurement systems (bal...
A typical educational wind tunnel need only measure the lift and drag forces and be able to control ...
M.Phil.In today's world with its competitive environment there is a need to shorten product developm...
Brief details of gauging work carried out on the\ud single component drag balance is discussed. The ...
An improved method of calibrating a wind-tunnel force balance involves the use of a unique load appl...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-s...