Analytical comparison of the acoustic analogy and Kirchhoff formulation for moving surfaces KS Brentner, F Farassat AIAA journal 36 (8), 1379-1386, 1998 | 741 | 1998 |
Modeling aerodynamically generated sound of helicopter rotors KS Brentner, F Farassat Progress in aerospace sciences 39 (2-3), 83-120, 2003 | 657 | 2003 |
Prediction of helicopter rotor discrete frequency noise: A computer program incorporating realistic blade motions and advanced acoustic formulation KS Brentner | 268 | 1986 |
Computational aeroacoustic analysis of slat trailing-edge flow BA Singer, DP Lockard, KS Brentner AIAA journal 38 (9), 1558-1564, 2000 | 171 | 2000 |
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 | 156 | 1998 |
Helicopter noise prediction: the current status and future direction KS Brentner, F Farassat Journal of Sound and Vibration 170 (1), 79-96, 1994 | 137 | 1994 |
High-accuracy algorithms for computational aeroacoustics DP Lockard, KS Brentner, HL Atkins AIAA journal 33 (2), 246-251, 1995 | 130 | 1995 |
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 | 122 | 1998 |
An efficient and robust method for predicting helicopter high-speed impulsive noise KS Brentner Journal of Sound and Vibration 203 (1), 87-100, 1997 | 119 | 1997 |
Maneuvering rotorcraft noise prediction GA Brès, KS Brentner, G Perez, HE Jones Journal of Sound and Vibration 275 (3-5), 719-738, 2004 | 117 | 2004 |
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 | 117 | 1988 |
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 | 102 | 2000 |
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 | 94 | 2009 |
An aeroacoustic analysis of wind turbines P Morris, L Long, K Brentner 42nd AIAA aerospace sciences meeting and exhibit, 1184, 2004 | 75 | 2004 |
Acoustic scattering in the time domain using an equivalent source method S Lee, KS Brentner, PJ Morris AIAA journal 48 (12), 2772-2780, 2010 | 70 | 2010 |
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 | 64 | 2002 |
Supersonic quadrupole noise theory for high-speed helicopter rotors F Farassat, KS Brentner Journal of Sound and Vibration 218 (3), 481-500, 1998 | 64 | 1998 |
Simulation of acoustic scattering from a trailing edge B Singer, K Brentner, D Lockard, G Lilley 37th Aerospace Sciences Meeting and Exhibit, 231, 1999 | 61 | 1999 |
Assessment of time-domain equivalent source method for acoustic scattering S Lee, KS Brentner, PJ Morris AIAA journal 49 (9), 1897-1906, 2011 | 53 | 2011 |
Challenges and opportunities for low noise electric aircraft E Greenwood, KS Brentner, RF Rau, ZF Ted Gan International Journal of Aeroacoustics 21 (5-7), 315-381, 2022 | 49 | 2022 |