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wind tunnelSoftware
The practical value of a wind tunnel which is not dependent solely on size or achievable Reynolds number was examined. Measurement, interpretative and evaluative procedures developed in small facilities were also studied
After completion of the required calibrations, the Dornier open-throat tunnel is now in operation. W...
The purpose of this report is to investigate the status and future projections for the question of s...
Domestic and foreign wind tunnel facilities are enumerated and their technical parameters are descri...
Requirements for new technologies in the area of civil aircraft design are mainly related to the hig...
Given here is a brief description of the Gottingen Wind Tunnel for the testing of aircraft models, p...
The goals, design, problems, and value of cryogenic transonic wind tunnels being developed in Europe...
A general description of the small DVL wind tunnel is provided, with emphasis on air conduction, blo...
Wind tunnel testing of helicopters, and test program for Polish helicopter industr
A brief overview is given of the National Full-scale Aerodynamics Complex. Its geometry, design, con...
In wind tunnel tests, the problems arise of determining the wall pressure distribution, calculating ...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
The wind tunnel is the most fundamental test equipment for aircraft testing and studying aerodynamic...
A review is presented of some of the lessons learned from wind tunnel tests since World War II. Wind...
International audienceThe paper aims at showing the evolution of methods to design a large wind tunn...
The contribution of wind tunnels to aerodynamic studies is described. The development of the wind tu...
After completion of the required calibrations, the Dornier open-throat tunnel is now in operation. W...
The purpose of this report is to investigate the status and future projections for the question of s...
Domestic and foreign wind tunnel facilities are enumerated and their technical parameters are descri...
Requirements for new technologies in the area of civil aircraft design are mainly related to the hig...
Given here is a brief description of the Gottingen Wind Tunnel for the testing of aircraft models, p...
The goals, design, problems, and value of cryogenic transonic wind tunnels being developed in Europe...
A general description of the small DVL wind tunnel is provided, with emphasis on air conduction, blo...
Wind tunnel testing of helicopters, and test program for Polish helicopter industr
A brief overview is given of the National Full-scale Aerodynamics Complex. Its geometry, design, con...
In wind tunnel tests, the problems arise of determining the wall pressure distribution, calculating ...
This report discusses the general considerations for the design of aerodynamic laboratories. The dim...
The wind tunnel is the most fundamental test equipment for aircraft testing and studying aerodynamic...
A review is presented of some of the lessons learned from wind tunnel tests since World War II. Wind...
International audienceThe paper aims at showing the evolution of methods to design a large wind tunn...
The contribution of wind tunnels to aerodynamic studies is described. The development of the wind tu...
After completion of the required calibrations, the Dornier open-throat tunnel is now in operation. W...
The purpose of this report is to investigate the status and future projections for the question of s...
Domestic and foreign wind tunnel facilities are enumerated and their technical parameters are descri...
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