Add to ORKGReport embodies a description of the balance designed and constructed for the use of the National Advisory Committee for Aeronautics at Langley Field, and also deals with the theory of sensitivity of balances and with the errors to which wind tunnel balances of various types are subject
The first International Symposium on Strain Gauge Balances was sponsored and held at NASA Langley Re...
A discussion on the fundamental concepts associated with wind tunnel forces measurement systems (bal...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
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...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
A flow-through balance is provided which includes a non-metric portion and a metric portion which fo...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
NASA Langley has a small, subsonic wind tunnel in use with the 13-inch Magnetic Suspension and Balan...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
The National Aeronautics and Space Administration (NASA) Langley Research Center (LaRC) has been des...
A typical educational wind tunnel need only measure the lift and drag forces and be able to control ...
Report discusses the theory of energy losses in wind tunnels, the application of the Drzewiecki theo...
The first International Symposium on Strain Gauge Balances was sponsored and held at NASA Langley Re...
A discussion on the fundamental concepts associated with wind tunnel forces measurement systems (bal...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
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...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
A flow-through balance is provided which includes a non-metric portion and a metric portion which fo...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
The vertical open-throat wind tunnel of the National Advisory Committee for Aeronautics is described...
NASA Langley has a small, subsonic wind tunnel in use with the 13-inch Magnetic Suspension and Balan...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
The National Aeronautics and Space Administration (NASA) Langley Research Center (LaRC) has been des...
A typical educational wind tunnel need only measure the lift and drag forces and be able to control ...
Report discusses the theory of energy losses in wind tunnels, the application of the Drzewiecki theo...
The first International Symposium on Strain Gauge Balances was sponsored and held at NASA Langley Re...
A discussion on the fundamental concepts associated with wind tunnel forces measurement systems (bal...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...