The most important aerodynamical qualities that should be aimed at in wind tunnel design, are as follows: 1) constant and parallel direction of flow; 2) uniform velocity across all sections; 3) absence of turbulent motion; 4) constant velocity of flow. The above-mentioned qualities are all realized in a high degree in the Gottingen type of wind tunnel, with a parallel portion before the working section, the cross section of which is steadily reduced. It is shown in what follows, that the system can be applied to other wind tunnels, such as the N.P.L. or Eiffel type
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
The wind tunnel is one of the oldest tools for research in !he field of aeronautical engineering. In...
Requirements for new technologies in the area of civil aircraft design are mainly related to the hig...
A brief nonmathematical outline is given of modern views as to the nature of the effect of turbulenc...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
Discussed here is a new type of wind tunnel, its advantages, the difficulties attendant upon its use...
The plans for the wind tunnel at Issey-les-Moulineaux are discussed in relation to concerns about th...
Now, in existing wind tunnels, using a horsepower of 100 to 300, the models are generally made to a ...
With the assistance and cooperation of the National Advisory Committee for Aeronautics the Bureau of...
Report discusses the theory of energy losses in wind tunnels, the application of the Drzewiecki theo...
A brief overview is given of the National Full-scale Aerodynamics Complex. Its geometry, design, con...
The use of exit cones and different blade configurations to reduce the motive power required in wind...
Many experimental arrangements of varying kind involve the problems of assuring a large, steady air ...
This Thesis has endorsed employing a novel indraft configuration for a severely spatially and financ...
Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1949.Bibliog...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
The wind tunnel is one of the oldest tools for research in !he field of aeronautical engineering. In...
Requirements for new technologies in the area of civil aircraft design are mainly related to the hig...
A brief nonmathematical outline is given of modern views as to the nature of the effect of turbulenc...
This report is a continuation of National Advisory Committee for Aeronautics report no. 73. The vari...
Discussed here is a new type of wind tunnel, its advantages, the difficulties attendant upon its use...
The plans for the wind tunnel at Issey-les-Moulineaux are discussed in relation to concerns about th...
Now, in existing wind tunnels, using a horsepower of 100 to 300, the models are generally made to a ...
With the assistance and cooperation of the National Advisory Committee for Aeronautics the Bureau of...
Report discusses the theory of energy losses in wind tunnels, the application of the Drzewiecki theo...
A brief overview is given of the National Full-scale Aerodynamics Complex. Its geometry, design, con...
The use of exit cones and different blade configurations to reduce the motive power required in wind...
Many experimental arrangements of varying kind involve the problems of assuring a large, steady air ...
This Thesis has endorsed employing a novel indraft configuration for a severely spatially and financ...
Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Aeronautical Engineering, 1949.Bibliog...
The causes of error in experiments conducted in wind tunnel tests are given and the value of in-flig...
The wind tunnel is one of the oldest tools for research in !he field of aeronautical engineering. In...
Requirements for new technologies in the area of civil aircraft design are mainly related to the hig...