Dr. Zahm's report is a description of the six-component wind-tunnel balance in use at the Aerodynamic Laboratory, Washington Navy Yard. The description of the balance gives the mechanical details and the method of operation, and is accompanied by line drawings showing the construction of the balance. The balance is of particular interest, as it allows the model to be set up quickly and accurately in roll, pitch, and yaw, without stopping the wind. It is possible to measure automatically, directly, and independently the drag, cross-wind force, and lift; also the rolling, pitching, and yawing moments. It is also possible to make the balance self-recording
The supersonic free-flight wind tunnel is a facility at the Ames Laboratory of the NACA in which aer...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
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...
The difficulties experienced in properly holding thin tipped or tapered airfoils while testing on an...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
This report combines the wind tunnel results of tests on four control surface models made in the two...
This report describes an electrical hinge-moment balance for use with wind-tunnel models of aircraft...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
A typical educational wind tunnel need only measure the lift and drag forces and be able to control ...
This report describes the layout of the laboratory along with the motor and balance for the wind tun...
M.Phil.In today's world with its competitive environment there is a need to shorten product developm...
Described here is an automatic control that has been used in several forms in wind tunnels at the Wa...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
The supersonic free-flight wind tunnel is a facility at the Ames Laboratory of the NACA in which aer...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...
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...
The difficulties experienced in properly holding thin tipped or tapered airfoils while testing on an...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
This report combines the wind tunnel results of tests on four control surface models made in the two...
This report describes an electrical hinge-moment balance for use with wind-tunnel models of aircraft...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
A typical educational wind tunnel need only measure the lift and drag forces and be able to control ...
This report describes the layout of the laboratory along with the motor and balance for the wind tun...
M.Phil.In today's world with its competitive environment there is a need to shorten product developm...
Described here is an automatic control that has been used in several forms in wind tunnels at the Wa...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
The supersonic free-flight wind tunnel is a facility at the Ames Laboratory of the NACA in which aer...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
Four N.A.C.A. 23012 wings were tested at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tu...