INCAS TRISONIC WIND TUNNEL

Journal Title: INCAS BULLETIN - Year 2009, Vol 1, Issue 1

Abstract

The 1.2 m x 1.2 m Trisonic Blowdown Wind Tunnel is the largest of the experimental facilities at the National Institute for Aerospace Research - I.N.C.A.S. "Elie Carafoli", Bucharest, Romania. The tunnel has been designed by the Canadian company DSMA (now AIOLOS) and since its commissioning in 1978 has performed high speed aerodynamic tests for more than 120 projects of aircraft, missiles and other objects among which the twin jet fighter IAR-93, the jet trainer IAR-99, the MIG-21 Lancer, the Polish jet fighter YRYDA and others. In the last years the wind tunnel has been used mostly for experimental research in European projects such as UFAST. The high flow quality parameters and the wide range of testing capabilities ensure the competitivity of the tunnel at an international level.

Authors and Affiliations

Florin MUNTEANU

Keywords

Related Articles

Neuro-fuzzy control synthesis for hydrostatic type servoactuators. Experimental results

Continuing recent works of the authors, the paper shows the developing and the application of a neuro-fuzzy control law to the positioning outer loop of a hydrostatic type servoactuator. Experimental results are presente...

Estimation of Wind Tunnel Corrections Using Potential Models

The evaluation of the tunnel correction remains an actual problem, especially for the effect of tunnel walls. Even if the experimental campaign meets the basic similitude criteria (Mach, Reynolds etc.), the wall effect o...

Design of Air Traffic Control Operation System

This paper presents a numerical simulation for a different aircraft, based on the specific aircraft data that can be incorporated in the model and the equations of motions which can be consequently solved. The aircraft f...

The unsteady turbulent flows structure study present status

The processes of heat transfer and hydraulic plays a very important role in the design and prototyping of aerospace technology. In most cases this technique works under significant unsteady conditions. Steady approach fo...

Modeling of Target Tracking System for Homing Missiles and Air Defense Systems

One reason of why the guidance and control systems are imperfect is due to the dynamics of both the tracker and the missile, which appears as an error in the alignment with the LOS and delay in the response of the missil...

Download PDF file
  • EP ID EP102782
  • DOI 10.13111/2066-8201.2009.1.1.2
  • Views 84
  • Downloads 0

How To Cite

Florin MUNTEANU (2009). INCAS TRISONIC WIND TUNNEL. INCAS BULLETIN, 1(1), 5-11. https://europub.co.uk/articles/-A-102782