28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
Paper ICAS 2012-3.9.3
COMPUTATIONAL STUDY ON NOISE GENERATION FROM A TWO-WHEEL MAIN LANDING GEAR
M. Murayama, Y. Yokokawa, K. Yamamoto
JAXA, Japan
Keywords: aeroacoustics, airframe noise, landing gear
In this paper, obtained knowledge and findings about the flow structures and possible noise sources around a two-wheel landing gear model by a series of steady and unsteady computations are discussed. The flowfields with several low noise devices are also investigated to clarify the noise reduction mechanism.
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