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PROCEDURE FOR THE DETERMINATION OF INER-TIAL AND GEOMETRICAL PARAMETERS OF AN AIRCRAFT ANGLE OF ATTACK PROBE FOR REQUIRED DAMPING
Mirko Kozić
A procedure for the determination of damping of a probe intended for measuring the angle of attack of low-speed aircraft has been presented as well as the analysis of effects of inertial and geometrical parameters on damping, which makes designing a probe with requested damping significantly easier. The number of wind tunnel tests is therefore reduced to the minimum since the only necessary procedure is to verify a chosen probe.
Ključne reči: Angle of attack probe, quasistationary flow, aeroelasticity, free damped oscillations, damping. |