Test Rig Adaptation for WT Measurements for OR&TP Configurations

Journal Title: INCAS BULLETIN - Year 2011, Vol 3, Issue 3

Abstract

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 shear stress distributions. To this purpose a model support system was designed which is not attached to the external balance but to the steel structure of the tunnel located outside the experimental room.

Authors and Affiliations

Adrian DOBRE

Keywords

Related Articles

Automation of the inner design of the aircraft

The task of forming the wind-swept surface according to the results of the aircraft’s inner design is described. The approach of the integration of natural and virtual prototyping in the design of equipment compartments...

Comparative Risk Assessment in Applicative Aerospace Projects using different approaches

Certification of the quality management system for aviation, space and defense organizations, according to EN 9100: 2016 / AS 9100D standard requires compliance with the operational risk management requirement. This arti...

Optimization of the flueric actuators testing system

A supplying system for air with precisely controlled temperature, pressure, flow and speed has been designed in order to test the flueric actuator. All these parameters are monitored and the acquired data are stored on a...

A new approximation of the dispersion relations occurring in the sound-attenuation problem of turbofan aircraft engines

The dispersion relations, appearing in the analysis of the stability of a gas flow in a straight acoustically-lined duct with respect to perturbations produced by a time harmonic source, beside the wave number and comple...

[b]Profiles with Coanda effect, necessaries to wind turbines[/b]

The air flow separation around profiles and the wind turbine rotor vibration leading to the blade breaking is a well known phenomenon based on which the present work is conceived. The paper is focused on theoretic and ex...

Download PDF file
  • EP ID EP129654
  • DOI 10.13111/2066-8201.2011.3.3.14
  • Views 62
  • Downloads 0

How To Cite

Adrian DOBRE (2011). Test Rig Adaptation for WT Measurements for OR&TP Configurations. INCAS BULLETIN, 3(3), 139-146. https://europub.co.uk/articles/-A-129654