Kenneth Steven Brentner

    • 2300 Citations
    • 22 h-Index
    1983 …2019

    Research output per year

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    2019

    Study of active rotor control for in-plane rotor noise reduction

    Yang, T., Brentner, K. S., Corle, E. & Schmitz, S., Jan 1 2019, In : Journal of Aircraft. 56, 1, p. 179-190 12 p.

    Research output: Contribution to journalArticle

    2018

    A dual compact model for rotor thickness noise prediction

    Yang, T., Brentner, K. S. & Walsh, G. D., Apr 1 2018, In : Journal of the American Helicopter Society. 63, 2, 022007.

    Research output: Contribution to journalArticle

    1 Scopus citations

    Surface roughness effect on rotor broadband noise

    Cheng, B., Han, Y., Brentner, K. S., Palacios, J., Morris, P. J., Hanson, D. & Kinzel, M., Jul 1 2018, In : International Journal of Aeroacoustics. 17, 4-5, p. 438-466 29 p.

    Research output: Contribution to journalArticle

    1 Scopus citations
    2017

    Application of synthetic array techniques for improved simulations of hot supersonic jet noise

    Nelson, C. C., Cain, A. B., Dougherty, R., Brentner, K. S. & Morris, P. J., Jul 1 2017, In : International Journal of Aeroacoustics. 16, 4-5, p. 382-402 21 p.

    Research output: Contribution to journalArticle

    2015

    A dual compact model for rotor noise prediction

    Yang, T., Brentner, K. S., Walsh, G. & Li, Y., Jan 1 2015, In : Annual Forum Proceedings - AHS International. 1, January, p. 32-46 15 p.

    Research output: Contribution to journalArticle

    2014

    A method for predicting the noise of a tip-jet driven rotor

    Brentner, K. S., MorrisG, P. J. & Lopes, L. V., Jul 2014, In : Journal of the American Helicopter Society. 59, 3, 032004.

    Research output: Contribution to journalArticle

    4 Scopus citations
    2012

    Time-domain approach for acoustic scattering of rotorcraft noise

    Lee, S., Brentner, K. S. & Morris, P. J., Oct 1 2012, In : Journal of the American Helicopter Society. 57, 4, 042001.

    Research output: Contribution to journalArticle

    22 Scopus citations
    2011

    Assessment of time-domain equivalent source method for acoustic scattering

    Lee, S., Brentner, K. S. & Morris, P. J., Sep 1 2011, In : AIAA journal. 49, 9, p. 1897-1906 10 p.

    Research output: Contribution to journalArticle

    31 Scopus citations
    2010

    Acoustic scattering in the time domain using an equivalent source method

    Lee, S., Brentner, K. S. & Morris, P. J., Dec 1 2010, In : AIAA journal. 48, 12, p. 2772-2780 9 p.

    Research output: Contribution to journalArticle

    44 Scopus citations

    Framework for a landing-gear model and acoustic prediction

    Lopes, L. V., Brentner, K. S. & Morris, P. J., May 1 2010, In : Journal of Aircraft. 47, 3, p. 763-774 12 p.

    Research output: Contribution to journalArticle

    11 Scopus citations

    Improved algorithm for nonlinear sound propagation with aircraft and helicopter noise applications

    Lee, S., Morris, P. J. & Brentner, K. S., Nov 1 2010, In : AIAA journal. 48, 11, p. 2586-2595 10 p.

    Research output: Contribution to journalArticle

    6 Scopus citations
    2009

    A method to predict acoustic scattering of rotorcraft noise

    Lee, S., Erwin, J. P. & Brentner, K. S., Oct 1 2009, In : Journal of the American Helicopter Society. 54, 4, 042007.

    Research output: Contribution to journalArticle

    12 Scopus citations

    Analytic formulation and numerical implementation of an acoustic pressure gradient prediction

    Lee, S., Brentner, K. S., Farassat, F. & Morris, P. J., Jan 23 2009, In : Journal of Sound and Vibration. 319, 3-5, p. 1200-1221 22 p.

    Research output: Contribution to journalArticle

    63 Scopus citations
    8 Scopus citations

    Time-domain approach for acoustic scattering of rotorcraft noise

    Lee, S., Brentner, K. S. & Morris, P. J., 2009, In : Annual Forum Proceedings - AHS International. 1, p. 579-591 13 p.

    Research output: Contribution to journalArticle

    6 Scopus citations
    2008

    A computational study of helicopter rotor wakes and noise generated during transient maneuvers

    Chen, H. N., Brentner, K. S., Ananthan, S. & Leishman, J. G., Jan 1 2008, In : Journal of the American Helicopter Society. 53, 1, p. 37-55 19 p.

    Research output: Contribution to journalArticle

    12 Scopus citations

    The effect of blade deformation rotorcraft acoustics

    Hennes, C. C. & Brentner, K. S., Oct 1 2008, In : Journal of the American Helicopter Society. 53, 4, p. 398-411 14 p.

    Research output: Contribution to journalArticle

    3 Scopus citations
    2006

    Acoustics 2006

    Hennes, C. C. & Brentner, K. S., Dec 1 2006, In : Vertiflite. 52, 4, p. 30-39 10 p.

    Research output: Contribution to journalArticle

    2005

    A first step toward the prediction of rotorcraft maneuver noise

    Perez, G., Brentner, K. S., Brès, G. A. & Jones, H. E., Jul 2005, In : Journal of the American Helicopter Society. 50, 3, p. 230-237 8 p.

    Research output: Contribution to journalArticle

    7 Scopus citations

    A subjective test of modulated blade spacing for helicopter main rotors

    Sullivan, B. M., Edwards, B. D., Brentner, K. S. & Booth, E. R., Jan 1 2005, In : Journal of the American Helicopter Society. 50, 1, p. 26-32 7 p.

    Research output: Contribution to journalArticle

    6 Scopus citations

    Development of a low-cost, multi-disciplinary rotorcraft simulation facility

    Horn, J. F., Bridges, D. O., Lopes, L. V. & Brentner, K. S., Jul 1 2005, In : Journal of Aerospace Computing, Information and Communication. 2, 7 JULY, p. 267-284 18 p.

    Research output: Contribution to journalArticle

    27 Scopus citations

    Investigation of soot combustion in underexpanded jet plume flows

    Viswanath, K., Brentner, K. S., Gimelshein, S. F. & Levin, D. A., Jan 1 2005, In : Journal of thermophysics and heat transfer. 19, 3, p. 282-293 12 p.

    Research output: Contribution to journalArticle

    10 Scopus citations

    Near real-time simulation of rotorcraft acoustics and flight dynamics

    Brentner, K. S., Lopes, L., Chen, H. N. & Horn, J. F., Jan 1 2005, In : Journal of Aircraft. 42, 2, p. 347-355 9 p.

    Research output: Contribution to journalArticle

    9 Scopus citations

    Predicted noise for a main rotor with modulated blade spacing

    Brentner, K. S., Edwards, B. D., Riley, R. & Schillings, J., Jan 1 2005, In : Journal of the American Helicopter Society. 50, 1, p. 18-25 8 p.

    Research output: Contribution to journalArticle

    12 Scopus citations
    2004

    Maneuvering rotorcraft noise prediction

    Brès, G. A., Brentner, K. S., Perez, G. & Jones, H. E., Aug 23 2004, In : Journal of Sound and Vibration. 275, 3-5, p. 719-738 20 p.

    Research output: Contribution to journalArticle

    87 Scopus citations
    2000

    Computational aeroacoustic analysis of slat trailing-edge flow

    Singer, B. A., Lockard, D. P. & Brentner, K. S., Sep 2000, In : AIAA journal. 38, 9, p. 1558-1564 7 p.

    Research output: Contribution to journalArticle

    118 Scopus citations

    Simulation of acoustic scattering from a trailing edge

    Singer, B. A., Brentner, K. S., Lockard, D. P. & Lilley, G. M., Feb 24 2000, In : Journal of Sound and Vibration. 230, 3, p. 541-560 20 p.

    Research output: Contribution to journalArticle

    67 Scopus citations
    1998

    Computation of vortex shedding and radiated sound for a circular cylinder: Subcritical to transcritical Reynolds numbers

    Cox, J. S., Brentner, K. S. & Rumsey, C. L., Jan 1 1998, In : Theoretical and Computational Fluid Dynamics. 12, 4, p. 233-253 21 p.

    Research output: Contribution to journalArticle

    96 Scopus citations

    Supersonic quadrupole noise theory for high-speed helicopter rotors

    Farassat, F. & Brentner, K. S., Dec 3 1998, In : Journal of Sound and Vibration. 218, 3, p. 481-500 20 p.

    Research output: Contribution to journalArticle

    43 Scopus citations

    The acoustic analogy and the prediction of the noise of rotating blades

    Farassat, F. & Brentner, K. S., Jan 1 1998, In : Theoretical and Computational Fluid Dynamics. 10, 1-4, p. 155-170 16 p.

    Research output: Contribution to journalArticle

    46 Scopus citations
    1997

    An efficient and robust method for computing quadrupole noise

    Brentner, K. S. & Holland, P. C., Apr 1 1997, In : Journal of the American Helicopter Society. 42, 2, p. 172-181 10 p.

    Research output: Contribution to journalArticle

    26 Scopus citations

    An efficient and robust method for predicting helicopter high-speed impulsive noise

    Brentner, K. S., May 29 1997, In : Journal of Sound and Vibration. 203, 1, p. 87-100 14 p.

    Research output: Contribution to journalArticle

    59 Scopus citations

    Numerical algorithms for acoustic integrals with examples for rotor noise prediction

    Brentner, K. S., Jan 1 1997, In : AIAA journal. 35, 4, p. 625-630 6 p.

    Research output: Contribution to journalArticle

    29 Scopus citations
    1995

    High-accuracy algorithms for computational aeroacoustics

    Lockard, D. P., Brentner, K. S. & Atkins, H. L., Feb 1995, In : AIAA journal. 33, 2, p. 246-251 6 p.

    Research output: Contribution to journalArticle

    80 Scopus citations
    1994

    Helicopter noise prediction: The current status and future direction

    Brentner, K. S. & Farassat, F., Feb 10 1994, In : Journal of Sound and Vibration. 170, 1, p. 79-96 18 p.

    Research output: Contribution to journalArticle

    51 Scopus citations

    Sensitivity of acoustic predictions to variation of input parameters

    Brentner, K. S., Burley, C. L. & Marcolini, M. A., Jul 1 1994, In : Journal of the American Helicopter Society. 39, 3, p. 43-52 10 p.

    Research output: Contribution to journalArticle

    15 Scopus citations
    1993

    Direct numerical calculation of acoustics: Solution evaluation through energy analysis

    Brentner, K. S., Jan 1 1993, In : Journal of Fluid Mechanics. 254, p. 267-281 15 p.

    Research output: Contribution to journalArticle

    6 Scopus citations
    1988

    Prediction of helicopter rotor discrete frequency noise for three scale models

    Brentner, K. S., May 1988, In : Journal of Aircraft. 25, 5, p. 420-427 8 p.

    Research output: Contribution to journalArticle

    4 Scopus citations

    USES AND ABUSES OF THE ACOUSTIC ANALOGY IN HELICOPTER ROTOR NOISE PREDICTION.

    Farassat, F. & Brentner, K. S., Jan 1 1988, In : Journal of the American Helicopter Society. 33, 1, p. 29-36 8 p.

    Research output: Contribution to journalArticle

    63 Scopus citations
    1983

    THEORETICAL AND EXPERIMENTAL INVESTIGATION OF SUPERSONIC AERODYNAMIC CHARACTERISTICS OF A TWIN-FUSELAGE CONCEPT.

    Wood, R. M., Miller, D. S. & Brentner, K. S., Jan 1 1983, In : NASA Technical Paper.

    Research output: Contribution to journalArticle

    1 Scopus citations