Acoustic Array Measurements in Aerodynamic Wind Tunnels : A Subspace Approach for Noise Suppression

Author(s):  
Jean Bulté
Author(s):  
Nathan J. Burnside ◽  
William C. Horne ◽  
Kevin R. Elmer ◽  
Rui Cheng ◽  
Leon Brusniak

2017 ◽  
Vol 16 (4-5) ◽  
pp. 326-357
Author(s):  
Nathan J Burnside ◽  
William C Horne ◽  
Kevin R Elmer ◽  
Rui Cheng ◽  
Leon Brusniak

Detailed acoustic measurements of the noise from the leading-edge Krueger flap of a 5.75% hybrid wing body aircraft model were acquired with a traversing phased microphone array in the Arnold Engineering Development Complex NFAC 40- by 80-foot wind tunnel. The spatial resolution of the array was sufficient to distinguish between individual support brackets over the full-scale frequency range of 100 to 2875 Hz. For conditions representative of landing and take-off configuration, the noise from the brackets dominated other sources near the leading edge. Inclusion of flight-like brackets for select conditions highlights the importance of including the correct number of leading-edge high-lift device brackets with sufficient scale and fidelity. These measurements support the development of a Krueger noise model which includes cove and bracket noise.


Author(s):  
Stefan Kroeber ◽  
Klaus Ehrenfried ◽  
Lars Koop ◽  
Andreas Lauterbach ◽  
Arne Henning

2021 ◽  
Vol 150 (1) ◽  
pp. 417-427
Author(s):  
Jianchao Ji ◽  
Cong Wang ◽  
Liang Wang ◽  
Song Fu

2000 ◽  
Author(s):  
Edward Awh ◽  
John Serences ◽  
Kelsey Libner ◽  
Michi Matsukura

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