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ACOUSTIC RADIATION FROM ROTATING BLADES—THE KIRCHHOFF METHOD IN AEROACOUSTICS

Journal of sound and vibration, 2001-01, Vol.239 (4), p.785-800

FARASSAT, F.

2001

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Modeling aerodynamically generated sound of helicopter rotors

Progress in aerospace sciences, 2003-02, Vol.39 (2), p.83-120

2003

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Analytic formulation and numerical implementation of an acoustic pressure gradient prediction

Journal of sound and vibration, 2009-01, Vol.319 (3), p.1200-1221

2009

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Broadband noise prediction when turbulence simulation is available—Derivation of Formulation 2B and its statistical analysis

Journal of sound and vibration, 2012-05, Vol.331 (10), p.2203-2208

2012

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Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces

AIAA journal, 1998-08, Vol.36 (8), p.1379-1386

1998

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Acoustic Analogy and Alternative Theories for Jet Noise Prediction

AIAA journal, 2002-04, Vol.40 (4), p.671-680

2002

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Broadband trailing edge noise predictions in the time domain

Journal of sound and vibration, 2004-03, Vol.271 (1), p.159-176

2004

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Nonstandard analysis and jump conditions for converging shock waves

Journal of mathematical physics, 2008-06, Vol.49 (6), p.063101-063101-18

2008

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Comments on the paper by Zinoviev and Bies “On acoustic radiation by a rigid object in a fluid flow”

Journal of sound and vibration, 2005-03, Vol.281 (3), p.1217-1223

Farassat, F.

2005

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THE INTEGRATION OF δ′(f) IN A MULTI-DIMENSIONAL SPACE

Journal of sound and vibration, 2000-02, Vol.230 (2), p.460-462

FARASSAT, F.

2000

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THE APPLICATION OF A BOUNDARY INTEGRAL EQUATION METHOD TO THE PREDICTION OF DUCTED FAN ENGINE NOISE

Journal of sound and vibration, 1999-11, Vol.227 (5), p.1019-1048

1999

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Reply by the Authors to C. K. W. Tam

AIAA journal, 2003-09, Vol.41 (9), p.1845-1847

2003

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Aircraft engine noise scattering by fuselage and wings: a computational approach

Journal of sound and vibration, 2003-05, Vol.263 (2), p.319-333

2003

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Extension of Kirchhoff's formula to radiation from moving surfaces

Journal of sound and vibration, 1988-06, Vol.123 (3), p.451-460

1988

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Linear Acoustic Formulas for Calculation of Rotating Blade Noise

AIAA journal, 1981-09, Vol.19 (9), p.1122-1130

Farassat, F

1981

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Further comments on the paper by Zinoviev and Bies, “On acoustic radiation by a rigid object in a fluid flow”

Journal of sound and vibration, 2006-02, Vol.290 (1), p.538-547

2006

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SUPERSONIC QUADRUPOLE NOISE THEORY FOR HIGH-SPEED HELICOPTER ROTORS

Journal of sound and vibration, 1998-12, Vol.218 (3), p.481-500

1998

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DUCTED-FAN ENGINE ACOUSTIC PREDICTIONS USING A NAVIER–STOKES CODE

Journal of sound and vibration, 1998-06, Vol.213 (4), p.643-664

1998

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A fast method of deriving the Kirchhoff formula for moving surfaces

The Journal of the Acoustical Society of America, 2007-11, Vol.122 (5_Supplement), p.2965-2965

2007

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The Acoustic Analogy and the Prediction of the Noise of Rotating Blades

Theoretical and computational fluid dynamics, 1998-01, Vol.10 (1-4), p.155-170

1998

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Multidimensional Generalized Functions in Aeroacoustics and Fluid Mechanics-Part 1: Basic Concepts and Operations

International journal of aeroacoustics, 2011-06, Vol.10 (2-3), p.161-199

2011

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A SIMPLE DERIVATION OF THE ACOUSTIC BOUNDARY CONDITION IN THE PRESENCE OF FLOW

Journal of sound and vibration, 1999-07, Vol.224 (2), p.384-386

1999

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Some Analytic Results for the Study of Broadband Noise Radiation from Wings, Propellers and Jets in Uniform Motion

International journal of aeroacoustics, 2003-07, Vol.2 (3), p.335-350

2003

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Helicopter Noise Prediction: The Current Status and Future Direction

Journal of sound and vibration, 1994-02, Vol.170 (1), p.79-96

1994

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Prediction of advanced propeller noise in the time domain

AIAA journal, 1986-04, Vol.24 (4), p.578-584

Farassat, F

1986

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ACOUSTIC RADIATION FROM ROTATING BLADES—THE KIRCHHOFF METHOD IN AEROACOUSTICS

Modeling aerodynamically generated sound of helicopter rotors

Analytic formulation and numerical implementation of an acoustic pressure gradient prediction

Broadband noise prediction when turbulence simulation is available—Derivation of Formulation 2B and its statistical analysis

Analytical Comparison of the Acoustic Analogy and Kirchhoff Formulation for Moving Surfaces

Acoustic Analogy and Alternative Theories for Jet Noise Prediction

Broadband trailing edge noise predictions in the time domain

Nonstandard analysis and jump conditions for converging shock waves

Comments on the paper by Zinoviev and Bies “On acoustic radiation by a rigid object in a fluid flow”

THE INTEGRATION OF δ′(f) IN A MULTI-DIMENSIONAL SPACE

THE APPLICATION OF A BOUNDARY INTEGRAL EQUATION METHOD TO THE PREDICTION OF DUCTED FAN ENGINE NOISE

Reply by the Authors to C. K. W. Tam

Aircraft engine noise scattering by fuselage and wings: a computational approach

Extension of Kirchhoff's formula to radiation from moving surfaces

Linear Acoustic Formulas for Calculation of Rotating Blade Noise

Further comments on the paper by Zinoviev and Bies, “On acoustic radiation by a rigid object in a fluid flow”

SUPERSONIC QUADRUPOLE NOISE THEORY FOR HIGH-SPEED HELICOPTER ROTORS

DUCTED-FAN ENGINE ACOUSTIC PREDICTIONS USING A NAVIER–STOKES CODE

A fast method of deriving the Kirchhoff formula for moving surfaces

The Acoustic Analogy and the Prediction of the Noise of Rotating Blades

Multidimensional Generalized Functions in Aeroacoustics and Fluid Mechanics-Part 1: Basic Concepts and Operations

A SIMPLE DERIVATION OF THE ACOUSTIC BOUNDARY CONDITION IN THE PRESENCE OF FLOW

Some Analytic Results for the Study of Broadband Noise Radiation from Wings, Propellers and Jets in Uniform Motion

Helicopter Noise Prediction: The Current Status and Future Direction

Prediction of advanced propeller noise in the time domain

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