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 analysis of results of wind-tunnel stability and control tests of powered airplane models in ter...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
This report describes the layout of the laboratory along with the motor and balance for the wind tun...
Results are presented for a series of tests made by the Advisory Committee's staff at Langley Field ...
Dr. Zahm's report is a description of the six-component wind-tunnel balance in use at the Aerodynami...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
This report outlines the flight conditions that are usually critical in determining the design of co...
This report is an analysis of two resistance equations which have particular application in the comp...
The 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
The analysis of results of wind-tunnel stability and control tests of powered airplane models in ter...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
This report describes the layout of the laboratory along with the motor and balance for the wind tun...
Results are presented for a series of tests made by the Advisory Committee's staff at Langley Field ...
Dr. Zahm's report is a description of the six-component wind-tunnel balance in use at the Aerodynami...
Report embodies a description of the balance designed and constructed for the use of the National Ad...
This report describes the redesigned variable-density wind tunnel of the National Advisory Committee...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
This report outlines the flight conditions that are usually critical in determining the design of co...
This report is an analysis of two resistance equations which have particular application in the comp...
The 6.C.1 balance is the first fully automatic balance assuring a continuous and simultaneous record...
This report contains the wind-tunnel test data obtained in the United States on a 36 by 6 inch R.A.F...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
This report groups in a uniform manner the aerodynamic properties of commonly used wing sections as ...
The analysis of results of wind-tunnel stability and control tests of powered airplane models in ter...
This report presents a description of the 7 by 10 foot wind tunnel and associated apparatus of the N...
This report describes the layout of the laboratory along with the motor and balance for the wind tun...