Trailing edge noise prediction from measured surface pressures

Journal of Sound and Vibration

Volumn 78, Issue 1, 1981, Pages 69-117

  Brooks, T F ^a   Hodgson, T H ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b NORTH CAROLINA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS;

EID: 0019875592     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/S0022-460X(81)80158-7     Document Type: Article

References (35)

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7. An experimental investigation of the trailing edge noise mechanism
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15. Noise source identification using coherent output power spectra
16. Use of coherence and phase data between two receivers in evaluation of noise environments
17. Time delay bias errors in estimating frequency response and coherence functions
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19. NACA Wartime Report L-682
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23. Modeling the wavevector-frequency spectrum of turbulent boundary layer wall pressure
24. The instantaneous structure of the wall pressure under a turbulent boundary layer flow
25. Measurements of the wave-number/phase velocity spectrum of wall pressure beneath a turbulent boundary layer
26. Some current research in unsteady fluid dynamics
27. Investigation of trailing edge noise
28. The importance of viscosity in experimental applications of Kirchhoff-type integral relations
29. An experimental evaluation of the application of the Kirchhoff formulation for sound radiation from an oscillating airfoil
30. Refraction of sound by a shear layer
31. American Institute of Aeronautics and Astronautics Paper No. 79-0628
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