28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-3.4.1
APPLICATION OF DYNAMIC PRESSURE MEASUREMENT FOR EMPENNAGE BUFFET
Keywords: vortex breakdown, pressure measurement, buffet, delta wing, twin tail
The paper describes development of Dynamic Pressure Measurement System for empennage buffet pressure measurements. An original Acoustic Calibration System has been developed and used for experimental validation and improvement of DPMS accuracy. The most significant parameters of empennage dynamic loading were investigated allowing for better understanding of aircraft buffet environment.
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