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DETERMINATION OF THE FLOW BENDING AN-GLE AT THE HORIZONTAL STABILIZER PLACE OF THE LASTA 95 AIRCRAFT
A method for experimental testing of the flow bending angle at the horizontal stabilizer place of the Lasta 95 aircraft model has been described. The testing was carried out in the subsonic wind tunnel T-35 for the steady flow rates of 50 and 100 m/s. The rear fuselage of the model was modified to carry a pyramidal probe holder instead of the horizontal stabilizer. The experimental results are presented and advantages and disadvantages of the method are analyzed.
Ključne reči: Subsonic flow, wind tunnel, pyramidal probe, flow quality. |