eawe phd-seminar, risø 4. october
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EAWE PhD-Seminar, Risø 4. October. PhD-Student Brian Riget Broe Semi-Empirical modeling of Aerodynamical Noise Risø National Laboratory Frederiksborgvej 399 4000 Roskilde, Denmark Aeroacoustics and Fluctuating Lift. Sources of aerodynamic noise. From Moriarty (2003). - PowerPoint PPT PresentationTRANSCRIPT
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EAWE PhD-Seminar, Risø 4. October
PhD-Student
Brian Riget Broe
Semi-Empirical modeling of Aerodynamical Noise
Risø National Laboratory
Frederiksborgvej 399
4000 Roskilde, Denmark
Aeroacoustics
and
Fluctuating Lift
EAWE PhD-Seminar, Risø 4.-5. October, 2006
Sources of aerodynamic noise
From Moriarty (2003)
EAWE PhD-Seminar, Risø 4.-5. October, 2006
Modeling the inflow noise
Model by Amiet (1975)
The power spectrum of the surface pressure
Task: Find the Fluctuating lift for an arbitrary profile
EAWE PhD-Seminar, Risø 4.-5. October, 2006
2-D gust on a flat plate
Sears (1941) and Graham (1971)
EAWE PhD-Seminar, Risø 4.-5. October, 2006
2-D gust on a flat plate, Results
A sinusoidal gust impinging on a semi-infinite flat plate. k is the wave vector which is in the plane of the flat plate. The wave vector has the component in the x-direction and in the y-direction. The wave front hits the edge of the plate in an angle. For the 1-D case is zero.
Sears (1941) 1-D
EAWE PhD-Seminar, Risø 4.-5. October, 2006
Measured surface pressure (1)
Measurements by Mish et al. (2006) for a NACA 0015 profile
EAWE PhD-Seminar, Risø 4.-5. October, 2006
Measured surface pressure (2)
Measurements by Mish et al. (2006) for a NACA 0015 profile
EAWE PhD-Seminar, Risø 4.-5. October, 2006
2-D gust on a profile
A sinusoidal gust impinging on a Joukowsky aerofoil. k is the wave vector. The wave vector has the component in the x-direction and in the z-direction. For the 1-D case is zero.
Goldstein and Atassi (1976)
EAWE PhD-Seminar, Risø 4.-5. October, 2006
Joint lift response of angle attack and camber
EAWE PhD-Seminar, Risø 4.-5. October, 2006
Lift response due to thickness
EAWE PhD-Seminar, Risø 4.-5. October, 2006
Summary
• A function for the fluctuating lift needs to be found for an arbitrary profile
• Measurements of the surface pressure is going to be made by Risø for a Risø profile
• Work on model by linearized theory to find the fluctuating lift due thickness
EAWE PhD-Seminar, Risø 4.-5. October, 2006
References
Listed in order of appearence• P. Moriarty and P. Migliore, Semi-Empirical Aeroacoustic Noise Prediction Code for Wind Tubines, 2003,
NREL/TP-500-34478.
• R. K. Amiet, Acoustic Radiation From An Airfoil In A Turbulent Stream, 1975, J. Sound and Vibr., 41(4), 407-420.
• P. F. Mish and W. J. Devenport, An experimental investigation of unsteady surface pressure on an airfoil in turbulence-Part 1: Effects of mean loading, 2006a, J. Sound and Vibr., 296, 417-446.
• W. R. Sears, Some Aspects of Non-Stationary Airfoil Theory and Its Practical Application, 1941, J. of the Aeronatical Sc., Vol. 8, No. 3, 104-108.
• J. M. R. Graham, Lifting Surface Theory for the Problem of an Arbitrarily Yawed Sinusoidal Gust Incident on a Thin Aerofoil in Imcompressible Flow, 1971, The Aeronautical Quart., 182-198.
• M. E. Goldstein and H. Atassi, A complete second-order theory for the unsteady flow about an airfoil due to a period gust, 1976, J. Fluid Mech., vol. 74, part 4, 741-765.
• H. M. Atassi, The Sears problem for a lifting airfoil revisited – new results, J. Fluid Mech., 1984, vol. 141, 109-122.