Wind tunnel models do not have complete similarity to the full scale airplane. Part of the dissimilarity is due to the difference between the stationary model in the artificial wind stream of the tunnel and the moving airplane in still air. There are a number of other reasons for departing from exact geometrical similitude. For reasons of accuracy and economy, all minor parts of the full scale airplane, such as struts, wires, fittings, control horns and other parts whose scale corrections are large are removed from wind tunnel models. By omitting the minor parts of the airplane in the wind tunnel model and adding to the forces and moments of the model those omitted parts measured full scale and properly reduced, the scale effects of such pa...
Detailed methods are presented for determining the corrections to results from wind-tunnel tests of ...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
Additional tests as recommended in reference 1 were made in the 7- by 10-foot wind tunnel of the 1/8...
Wind tunnel models do not have complete similarity to the full scale airplane. Part of the dissimila...
Here, it is shown that the construction of an airplane model can and should be simplified in order t...
In order to clear up the matter ( In the Spanish report it was stated that the reference surface for...
This paper was delivered before the Royal Aeronautical Society as the 1925 Wilbur Wright Memorial le...
This report gives a complete description of the full-scale wind tunnel of the National Advisory Comm...
To apply the experimental data measured in a wind tunnel for a scaled aircraft to a free-flying mode...
In the early stages of an aerodynamic development programme of a road vehicle it is common to use wi...
Low Mach number longitudinal-stability and control characteristics as predicted by use of wind tunne...
Calculations of the magnitude of the correction factors and the range of their variations for wind t...
Scaling criteriato be fulfilled to ensure dynamic similarity between full-scale flight conditions an...
This final year project is about Fabrication of wind tunnel in desktop size.Wind tunnel Wind tunnel ...
Scaling criteria to be fulfilled to ensure dynamic similarity between full-scale flight conditions a...
Detailed methods are presented for determining the corrections to results from wind-tunnel tests of ...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
Additional tests as recommended in reference 1 were made in the 7- by 10-foot wind tunnel of the 1/8...
Wind tunnel models do not have complete similarity to the full scale airplane. Part of the dissimila...
Here, it is shown that the construction of an airplane model can and should be simplified in order t...
In order to clear up the matter ( In the Spanish report it was stated that the reference surface for...
This paper was delivered before the Royal Aeronautical Society as the 1925 Wilbur Wright Memorial le...
This report gives a complete description of the full-scale wind tunnel of the National Advisory Comm...
To apply the experimental data measured in a wind tunnel for a scaled aircraft to a free-flying mode...
In the early stages of an aerodynamic development programme of a road vehicle it is common to use wi...
Low Mach number longitudinal-stability and control characteristics as predicted by use of wind tunne...
Calculations of the magnitude of the correction factors and the range of their variations for wind t...
Scaling criteriato be fulfilled to ensure dynamic similarity between full-scale flight conditions an...
This final year project is about Fabrication of wind tunnel in desktop size.Wind tunnel Wind tunnel ...
Scaling criteria to be fulfilled to ensure dynamic similarity between full-scale flight conditions a...
Detailed methods are presented for determining the corrections to results from wind-tunnel tests of ...
Report deals with the methods of constructing aerofoils and all other parts of a model airplane, inc...
Additional tests as recommended in reference 1 were made in the 7- by 10-foot wind tunnel of the 1/8...