The need to test large models at maximum speed regimes close to 100 m/s, for which the aerodynamic forces and moments occurring on the model far exceed the measuring capability of the existing TEM external balance, made it necessary to design an alternative model support system installed outside the INCAS subsonic wind tunnel. This is the case of models included in the Clean Sky European programs GRA and SFWA ITD. The wingspan of these models is equal to the width of the test section. For these models, the pressure distributions on the model surface should be determined by pressure measurement through small orifices connected to scanning devices while the aerodynamic forces and moments will be obtained by integration of the pressure and she...
Wind Tunnel measurements are conducted using scaled down models of aerospace as well as automotive s...
In this report the tasks performed by Dasa-M in support of the TST wind tunnel tests during phase 4 ...
Published results for standard wind tunnel models at non-standard test conditions are quite rare and...
The 2D Turbo Prop wing is part of the European Clean Sky JTI GRA Low Noise programme. For this, the ...
Wind tunnels are used to test scale-model air frames in order to collect aerodynamic data. The Subso...
Together with progress and enhancement of flight vehicles, requirements imposed on a level of ongrou...
The models for force and pressure measurements in 4-ft. Trisonic Wind Tunnel are generally mounted o...
For the purpose of establishing and validating aerodynamic performance predictions at transonic Mach...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...
This article presents a simplified computational fluid dynamics (CFD) model of the European Transoni...
The paper consists of two parts devoted correspondingly to the experimental opportunities and result...
This report describes a test rig designed for testing afterbody models of various aerospace vehicles...
A 1/8-scale model of a fan-in-wing concept was tested in the Langley 14- by 22-Foot Subsonic Tunnel....
A test rig and a strain gauge balance for high angle of attack flow have been developed for wind-tun...
Wind Tunnel measurements are conducted using scaled down models of aerospace as well as automotive s...
In this report the tasks performed by Dasa-M in support of the TST wind tunnel tests during phase 4 ...
Published results for standard wind tunnel models at non-standard test conditions are quite rare and...
The 2D Turbo Prop wing is part of the European Clean Sky JTI GRA Low Noise programme. For this, the ...
Wind tunnels are used to test scale-model air frames in order to collect aerodynamic data. The Subso...
Together with progress and enhancement of flight vehicles, requirements imposed on a level of ongrou...
The models for force and pressure measurements in 4-ft. Trisonic Wind Tunnel are generally mounted o...
For the purpose of establishing and validating aerodynamic performance predictions at transonic Mach...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
Wind tunnel is a device which plays the important role in the study of effect of a moving object thr...
This article presents a simplified computational fluid dynamics (CFD) model of the European Transoni...
The paper consists of two parts devoted correspondingly to the experimental opportunities and result...
This report describes a test rig designed for testing afterbody models of various aerospace vehicles...
A 1/8-scale model of a fan-in-wing concept was tested in the Langley 14- by 22-Foot Subsonic Tunnel....
A test rig and a strain gauge balance for high angle of attack flow have been developed for wind-tun...
Wind Tunnel measurements are conducted using scaled down models of aerospace as well as automotive s...
In this report the tasks performed by Dasa-M in support of the TST wind tunnel tests during phase 4 ...
Published results for standard wind tunnel models at non-standard test conditions are quite rare and...