Philip John Morris, PhD

    • 3704 Citations
    • 30 h-Index
    1969 …2019
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    Research Output 1969 2019

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    Conference contribution
    2019
    1 Citation (Scopus)

    Aeroacoustic performance of multi-stream, rectangular, supersonic jets

    Hromisin, S. M., Akatsuka, J., McLaughlin, D. K. & Morris, P. J., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Aeroacoustics
    Bypass ratio
    Turbofan engines
    Acoustic fields
    Noise abatement

    Effect of fluid inserts on low order models of jet noise reduction

    Prasad, C. & Morris, P. J., Jan 1 2019, 25th AIAA/CEAS Aeroacoustics Conference, 2019. [publishername] American Institute of Aeronautics and Astronautics Inc, AIAA, (25th AIAA/CEAS Aeroacoustics Conference, 2019).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    jet aircraft noise
    Die casting inserts
    inserts
    Noise abatement
    noise reduction

    Effects of nozzle configuration and bypass ratio on the aeroacoustics of dual stream supersonic jets

    Hromisin, S. M., McLaughlin, D. K. & Morris, P. J., Jan 1 2019, 25th AIAA/CEAS Aeroacoustics Conference, 2019. [publishername] American Institute of Aeronautics and Astronautics Inc, AIAA, (25th AIAA/CEAS Aeroacoustics Conference, 2019).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    bypass ratio
    Bypass ratio
    Aeroacoustics
    aeroacoustics
    nozzles

    Experimental and numerical investigation of jet noise reduction using fluid inserts for rectangular nozzle with aspect ratio of 2

    Akatsuka, J., Hromisin, S. M., McLaughlin, D. K. & Morris, P. J., Jan 1 2019, 25th AIAA/CEAS Aeroacoustics Conference, 2019. [publishername] American Institute of Aeronautics and Astronautics Inc, AIAA, (25th AIAA/CEAS Aeroacoustics Conference, 2019).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    jet aircraft noise
    Die casting inserts
    inserts
    Noise abatement
    noise reduction

    Investigation of high-order cell-centered finite difference method for aeroacoustics

    Jin, Y., Liao, F., Cai, J. & Morris, P. J., Jan 1 2019, 25th AIAA/CEAS Aeroacoustics Conference, 2019. [publishername] American Institute of Aeronautics and Astronautics Inc, AIAA, (25th AIAA/CEAS Aeroacoustics Conference, 2019).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Aeroacoustics
    aeroacoustics
    Finite difference method
    airfoils
    Airfoils

    Mean flow measurements in supersonic jets with noise reduction devices

    Akatsuka, J., Hromisin, S. M., Falcone, J., McLaughlin, D. K. & Morris, P. J., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Flow measurement
    Noise abatement
    Die casting inserts
    Fluids
    Flow structure
    2 Citations (Scopus)

    Unsteady simulations of fluid inserts for supersonic jet noise reduction

    Prasad, C. & Morris, P. J., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Die casting inserts
    Noise abatement
    Fluids
    Flow fields
    Nozzles
    2018

    Analysis of fluid insert noise reduction method with PIV

    Morgan, J., Shoemaker, C., McLaughlin, D. K., Morris, P. J. & Berger, Z. P., Jan 1 2018, 2018 AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3610. (2018 AIAA/CEAS Aeroacoustics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Die casting inserts
    Noise abatement
    Velocity measurement
    Flow fields
    Fluids

    Supersonic active noise reduction in small- and moderate-scale nozzles

    Morgan, J., McLaughlin, D. K. & Morris, P. J., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Noise abatement
    Nozzles
    Supersonic aircraft
    Aircraft engines
    2017
    9 Citations (Scopus)

    Experimental results for supersonic jet noise reduction using nozzle fluidic inserts

    Morgan, J., McLaughlin, D. K. & Morris, P. J., Jan 1 2017, 23rd AIAA/CEAS Aeroacoustics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, (23rd AIAA/CEAS Aeroacoustics Conference, 2017).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Noise abatement
    Nozzles
    Engines
    Air

    Extending on-demand noise reduction technology to military-style nozzles with 6 fluidic corrugations

    Hromisin, S. M., Powers, R. W., McLaughlin, D. K. & Morris, P. J., Jan 1 2017, 23rd AIAA/CEAS Aeroacoustics Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, (23rd AIAA/CEAS Aeroacoustics Conference, 2017).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Noise abatement
    Nozzles
    Acoustic fields
    Experiments
    9 Citations (Scopus)

    Further development of supersonic jet noise reduction using nozzle fluidic inserts

    Morgan, J., McLaughlin, D. K., Morris, P. J. & Prasad, C., Jan 1 2017, AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA 2017-0683. (AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Noise abatement
    Nozzles
    Aviation
    Experiments
    1 Citation (Scopus)

    The far-field acoustics of supersonic single and dual impinging jets with correlations to near-field noise

    Hromisin, S. M., Myers, L. M., McLaughlin, D. K. & Morris, P. J., Jan 1 2017, AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., AIAA 2017-0229. (AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Acoustic fields
    Acoustic noise
    Microphones
    Acoustic field measurement
    Acoustic waves
    2016
    1 Citation (Scopus)

    A comparison of the aeroacoustic characteristics of free and impinging jets with deflected seals noise reduction technique

    Hromisin, S. M., Myers, L. M., McLaughlin, D. K. & Morris, P. J., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (54th AIAA Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Aeroacoustics
    Noise abatement
    Seals
    Nozzles
    Military aircraft
    2 Citations (Scopus)

    Experimental and numerical study of fluidic corrugation design for supersonic jet noise reduction

    Hromisin, S. M., Lampenfield, J., McLaughlin, D. K. & Morris, P. J., Jan 1 2016, 22nd AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Noise abatement
    Nozzles
    Experiments
    Blow molding
    5 Citations (Scopus)

    Extending on-demand noise reduction to industry-scale models for tactical aircraft

    McLaughlin, D. K., Morris, P. J., Martens, S. & Lariviere, E. L., Jan 1 2016, 22nd AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Noise abatement
    Aircraft
    Fluidics
    Aircraft carriers
    Industry
    9 Citations (Scopus)

    Mean velocity and turbulence measurements of supersonic jets with fluidic inserts

    Powers, R. W., Hromisin, S. M., McLaughlin, D. K. & Morris, P. J., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (54th AIAA Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Turbulence
    Noise abatement
    Nozzles
    Flow fields
    7 Citations (Scopus)

    Noise reduction with fluidic inserts in supersonic jets exhausting over a simulated aircraft carrier deck

    Powers, R. W., McLaughlin, D. K. & Morris, P. J., Jan 1 2016, 21st AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (21st AIAA/CEAS Aeroacoustics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Aircraft carriers
    Fluidics
    Noise abatement
    Acoustic waves
    Microphones
    9 Citations (Scopus)

    Numerical simulations for supersonic jet noise reduction using fluidic inserts

    Kapusta, M., Powers, R., Morris, P. J. & McLaughlin, D. K., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (54th AIAA Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Noise abatement
    Computer simulation
    Nozzles
    Blow molding
    3 Citations (Scopus)

    Rotor broadband noise due to surface roughness during ice accretion

    Cheng, B., Han, Y., Brentner, K. S., Palacios, J., Morris, P. J., Hanson, D. & Kinzel, M., Jan 1 2016, 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, (54th AIAA Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Ice
    Rotors
    Surface roughness
    Boundary layers
    Turbulence
    2015
    4 Citations (Scopus)

    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., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0507. (53rd AIAA Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Microphones
    Computational fluid dynamics
    10 Citations (Scopus)

    Noise reduction in supersonic jets from rectangular convergent-divergent nozzles

    Powers, R. W., McLaughlin, D. K. & Morris, P. J., Jan 1 2015, 53rd AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2015-0231. (53rd AIAA Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Noise abatement
    Nozzles
    Fluidics
    Blow molding
    2014

    Accurate and efficient jet flow and noise simulations using the CDE (Compact Disturbance Equations)

    Du, Y. & Morris, P. J., Jan 1 2014, 20th AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics Inc., (20th AIAA/CEAS Aeroacoustics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Large eddy simulation
    Navier Stokes equations
    Euler equations
    Computational efficiency
    Turbulent flow

    Design and analysis of a supersonic jet noise reduction concept

    Pilony, A. R., Powers, U. W., McLaughlin, D. K. & Morris, P. J., Jan 1 2014, 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc., (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    jet aircraft noise
    Noise abatement
    noise reduction
    exhaust nozzles
    takeoff
    2 Citations (Scopus)

    Design and analysis of a supersonic jet noise reduction concept

    Pilon, A. R., Powers, R. W., McLaughlin, D. K. & Morris, P. J., Jan 1 2014, 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., (52nd Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Noise abatement
    Takeoff
    Seals
    Nozzles
    Exhaust systems (engine)
    1 Citation (Scopus)

    Numerical simulation of the effect of a low bypass cooling stream on supersonic jet noise

    Du, Y. & Morris, P. J., Jan 1 2014, 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. American Institute of Aeronautics and Astronautics Inc., (52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    jet aircraft noise
    bypasses
    bypass
    nozzles
    Nozzles

    Numerical simulation of the effect of a low bypass cooling stream on supersonic jet noise

    Du, Y. & Morris, P. J., Jan 1 2014, 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., (52nd Aerospace Sciences Meeting).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Nozzles
    Cooling
    Wave packets
    Computer simulation
    Fans
    3 Citations (Scopus)

    Optimization of blowing in a convergent-divergent nozzle for noise reduction

    Sikarwar, N. & Morris, P. J., Jan 1 2014, 20th AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics Inc., (20th AIAA/CEAS Aeroacoustics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Blow molding
    Noise abatement
    Nozzles
    Pressure distribution
    Aeroacoustics
    10 Citations (Scopus)

    Prediction, experiments and optimization of High-Speed jet noise reduction using fluidic inserts

    Morris, P. J., McLaughlin, D. K., Powers, R. & Kapusta, M., Jan 1 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014. American Institute of Aeronautics and Astronautics Inc., (50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Noise abatement
    Experiments
    Nozzles
    Vorticity
    3 Citations (Scopus)

    Quantification of rotor surface roughness due to ice accretion via broadband noise measurement

    Cheng, B., Han, Y., Brentner, K. S., Palacios, J. L. & Morris, P. J., Jan 1 2014, 70th American Helicopter Society International Annual Forum 2014. American Helicopter Society, p. 2680-2692 13 p. (Annual Forum Proceedings - AHS International; vol. 4).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Ice
    Rotors
    Surface roughness
    Sand
    Acoustics
    20 Citations (Scopus)

    Supersonic jet noise reduction by nozzle fluidic inserts with simulated forward flight

    Powers, R. W., McLaughlin, D. K., Morris, P. J. & Kuo, C. W., Jan 1 2014, 20th AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics Inc., (20th AIAA/CEAS Aeroacoustics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Fluidics
    Noise abatement
    Nozzles
    Military aircraft
    Die casting inserts
    2013
    3 Citations (Scopus)

    A new block interface condition for aeroacoustic applications

    Du, Y. & Morris, P. J., Sep 16 2013, 19th AIAA/CEAS Aeroacoustics Conference. 1 p.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Aeroacoustics
    aeroacoustics
    information flow
    communicating
    mesh
    3 Citations (Scopus)

    Application of synthetic phased array techniques to hot supersonic jet noise

    Nelson, C. C., Cain, A. B., Dougherty, R., Brentner, K. S. & Morris, P. J., Aug 19 2013, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013. (51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    synthetic arrays
    jet aircraft noise
    phased arrays
    Microphones
    charge flow devices
    11 Citations (Scopus)

    Experimental investigation of near-field pressure fluctuations generated by supersonic jets

    Kuo, C. W., Buisson, Q., McLaughlin, D. K. & Morris, P. J., Sep 16 2013, 19th AIAA/CEAS Aeroacoustics Conference. 1 p.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    near fields
    Microphones
    microphones
    Decomposition
    decomposition
    4 Citations (Scopus)

    Toward efficient computational aeroacoustic analysis of high speed jets

    Nelson, C., Cain, A., Du, Y., Morris, P. J. & Spyropoulos, J., Dec 17 2013, ASME Turbo Expo 2013: Turbine Technical Conference and Exposition, GT 2013. (Proceedings of the ASME Turbo Expo; vol. 2).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Computational aeroacoustics
    Aeroacoustics
    Acoustics
    8 Citations (Scopus)

    Validation of a time-domain equivalent source method for acoustic scattering by an oblate spheroid

    Cheng, B., Brentner, K. S. & Morris, P. J., Aug 19 2013, 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013. (51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    oblate spheroids
    acoustic scattering
    acoustics
    Acoustics
    scattering
    2012
    1 Citation (Scopus)

    Adjoint design methods for nozzles for reduced noise in high-speed jets

    Morris, P. J., Sikarwar, N., McLaughlin, D. K., Kuo, C. W. & Lurie, M., Dec 1 2012, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012. (48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Noise abatement
    Nozzles
    Cost functions
    Nozzle design
    Military aircraft
    2 Citations (Scopus)

    Noise predictions for high subsonic single and dual-stream jets in flight

    Saxena, S. & Morris, P. J., 2012, 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    noise prediction
    convergent nozzles
    Nozzles
    nozzles
    flight
    12 Citations (Scopus)

    Noise reduction in supersonic jets by nozzle fluidic inserts

    Kuo, C. W., Morris, P. J. & McLaughlin, D. K., Dec 1 2012, 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference). (18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    fluidics
    Fluidics
    inserts
    Noise abatement
    noise reduction
    2011
    4 Citations (Scopus)

    Noise simulations of supersonic hot jets for chevron nozzles

    Du, Y. & Morris, P. J., Dec 1 2011, 17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference). (17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference)).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    jet flow
    nozzles
    Nozzles
    nozzle geometry
    mesh
    1 Citation (Scopus)

    Simulations and measurements of the flow and noise in hot supersonic jets

    Morris, P. J., McLaughlin, D. K., Du, Y. & Kuo, C. W., Dec 1 2011, ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011. p. 111-125 15 p. (Proceedings of the ASME Turbo Expo; vol. 1).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Nozzles
    Acoustic fields
    Military aircraft
    Aircraft engines
    Computer simulation

    Supersonic jet flow and noise simulations of military-style baseline and chevron nozzles

    Du, Y. & Morris, P. J., Dec 1 2011, 40th International Congress and Exposition on Noise Control Engineering 2011, INTER-NOISE 2011. p. 369-377 9 p. (40th International Congress and Exposition on Noise Control Engineering 2011, INTER-NOISE 2011; vol. 1).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    supersonic jet flow
    jet aircraft noise
    nozzles
    jet exhaust
    multiblock grids
    4 Citations (Scopus)

    The prediction of broadband shock-associated noise including propagation effects

    Miller, S. A. E. & Morris, P. J., Dec 1 2011, 17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference). (17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference)).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    noise propagation
    Acoustic noise
    Green's function
    Green's functions
    shock

    Trailing-edge noise prediction using the non-linear disturbance equations

    Christiansen, M. D., Morris, P. J. & Brentner, K. S., Dec 1 2011, 17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference). (17th AIAA/CEAS Aeroacoustics Conference 2011 (32nd AIAA Aeroacoustics Conference)).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    noise prediction
    trailing edges
    Wind turbines
    Boundary layers
    disturbances
    2010
    2 Citations (Scopus)

    Assessment of time-domain equivalent source method for acoustic scattering

    Lee, S., Brentner, K. S. & Morris, P. J., Dec 6 2010, 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference). 2010-3821. (16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    acoustic scattering
    Acoustics
    Scattering
    Acoustic waves
    Acoustic intensity
    21 Citations (Scopus)

    High-resolution continuous scan acoustical holography applied to high-speed jet noise

    Vold, H., Shah, P. N., Davis, J., Bremner, P. G., McLaughlin, D., Morris, P. J., Veltin, J. & McKinley, R., Dec 6 2010, 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference). 2010-3754. (16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    acoustical holography
    jet aircraft noise
    Holography
    Microphones
    microphones
    7 Citations (Scopus)

    Nonlinear acoustic propagation predictions with applications to aircraft and helicopter noise

    Lee, S., Morris, P. J. & Brentner, K. S., Dec 13 2010, 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010-1384. (48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Cutoff frequency
    Helicopters
    Acoustics
    Aircraft
    Jet engines
    7 Citations (Scopus)

    The prediction of broadband shock-associated noise from dualstream and rectangular jets using RANS CFD

    Miller, S. A. E. & Morris, P. J., Dec 6 2010, 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference). 2010-3730. (16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    charge flow devices
    Computational fluid dynamics
    shock
    broadband
    predictions
    9 Citations (Scopus)

    Two component velocity correlations in jets and noise source modeling

    Morris, P. J. & Zaman, K. B. M. Q., Dec 6 2010, 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference). 2010-3781. (16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    probes
    Wire
    hot-wire anemometers
    statistical correlation
    interference
    2009
    3 Citations (Scopus)

    Airframe noise prediction with installed landing gear for a complete aircraft

    Lopes, L. V., Brentner, K. S. & Morris, P. J., 2009, 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference). 2009-3155

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Landing gear (aircraft)
    Airframes
    Aircraft
    Acoustic noise
    Acoustics