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Kenneth S. Brentner
Kenneth S. Brentner
Professor of Aerospace Engineering, The Pennsylvania State University
Verified email at psu.edu
Title
Cited by
Cited by
Year
Analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces
KS Brentner, F Farassat
AIAA journal 36 (8), 1379-1386, 1998
7331998
Modeling aerodynamically generated sound of helicopter rotors
KS Brentner, F Farassat
Progress in aerospace sciences 39 (2-3), 83-120, 2003
6372003
Prediction of helicopter rotor discrete frequency noise: A computer program incorporating realistic blade motions and advanced acoustic formulation
KS Brentner
2601986
Computational aeroacoustic analysis of slat trailing-edge flow
BA Singer, DP Lockard, KS Brentner
AIAA journal 38 (9), 1558-1564, 2000
1692000
Computation of vortex shedding and radiated sound for a circular cylinder: subcritical to transcritical Reynolds numbers
JS Cox, KS Brentner, CL Rumsey
Theoretical and Computational Fluid Dynamics 12, 233-253, 1998
1531998
Helicopter noise prediction: The current status and future direction
KS Brentner, F Farassat
Journal of Sound and Vibration 170 (1), 79-96, 1994
1351994
High-accuracy algorithms for computational aeroacoustics
DP Lockard, KS Brentner, HL Atkins
AIAA journal 33 (2), 246-251, 1995
1301995
The acoustic analogy and the prediction of the noise of rotating blades
F Farassat, KS Brentner
Theoretical and computational fluid dynamics 10 (1), 155-170, 1998
1191998
An efficient and robust method for predicting helicopter high-speed impulsive noise
KS Brentner
Journal of Sound and Vibration 203 (1), 87-100, 1997
1171997
The uses and abuses of the acoustic analogy in helicopter rotor noise prediction
F Farassat, KS Brentner
Journal of the American Helicopter Society 33 (1), 29-36, 1988
1151988
Maneuvering rotorcraft noise prediction
GA Brès, KS Brentner, G Perez, HE Jones
Journal of Sound and Vibration 275 (3-5), 719-738, 2004
1142004
Simulation of acoustic scattering from a trailing edge
BA Singer, KS Brentner, DP Lockard, GM Lilley
Journal of Sound and Vibration 230 (3), 541-560, 2000
1022000
Analytic formulation and numerical implementation of an acoustic pressure gradient prediction
S Lee, KS Brentner, F Farassat, PJ Morris
Journal of Sound and Vibration 319 (3-5), 1200-1221, 2009
902009
An aeroacoustic analysis of wind turbines
P Morris, L Long, K Brentner
42nd AIAA aerospace sciences meeting and exhibit, 1184, 2004
752004
Acoustic scattering in the time domain using an equivalent source method
S Lee, KS Brentner, PJ Morris
AIAA journal 48 (12), 2772-2780, 2010
672010
Supersonic quadrupole noise theory for high-speed helicopter rotors
F Farassat, KS Brentner
Journal of Sound and Vibration 218 (3), 481-500, 1998
631998
Maneuvering rotorcraft noise prediction: A new code for a new problem
KS Brentner, GA Bres, G Perez, HE Jones
Ahs aerodynamics, acoustics and test evaluation specialist meeting, 2002
622002
Simulation of acoustic scattering from a trailing edge
B Singer, K Brentner, D Lockard, G Lilley
37th Aerospace Sciences Meeting and Exhibit, 231, 1999
601999
Assessment of time-domain equivalent source method for acoustic scattering
S Lee, KS Brentner, PJ Morris
AIAA journal 49 (9), 1897-1906, 2011
512011
Noise prediction for maneuvering rotorcraft
K Brentner, H Jones
6th Aeroacoustics Conference and Exhibit, 2031, 2000
462000
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