Phillip Joseph, MD

2025

• Aeroacoustic Source Mechanisms of Fixed-Wing VTOL Configuration at Takeoff Hover

  Chaitanya P, Corbishley T, Palleja-Cabre S, Cho M, Karimian A, Joseph P, Akiwate D, Westcott O, Krishna S. Aeroacoustic Source Mechanisms of Fixed-Wing VTOL Configuration at Takeoff Hover. Drones 2025, 9: 864. DOI: 10.3390/drones9120864.

  Peer-Reviewed Original Research

  Concepts

• Propeller tonal noise reductions through synchrophasing: Mechanisms and performance

  Joseph P, Chaitanya P, Elliott S, Bhardwaj M, Chong T. Propeller tonal noise reductions through synchrophasing: Mechanisms and performance. Journal Of Sound And Vibration 2025, 610: 119110. DOI: 10.1016/j.jsv.2025.119110.

  Peer-Reviewed Original Research

  Citations

  Concepts

• On the slit trailing edges for aerofoil self-noise reduction

  Woodhead P, Chong T, Joseph P, Wissink J, Chaitanya P. On the slit trailing edges for aerofoil self-noise reduction. Journal Of Fluid Mechanics 2025, 1015: a43. DOI: 10.1017/jfm.2025.10370.

  Peer-Reviewed Original Research

  Citations

  Altmetric

  Concepts

• On the Mechanisms of Trailing Edge Noise Reduction by Upstream Treatments

  Sha S, Paruchuri C, Joseph P. On the Mechanisms of Trailing Edge Noise Reduction by Upstream Treatments. 2025 DOI: 10.2514/6.2025-3272.

  Peer-Reviewed Original Research

• On the Validity of Blade Response Functions for High Amplitude Vortical Gust

  Cho M, Paruchuri C, Joseph P. On the Validity of Blade Response Functions for High Amplitude Vortical Gust. 2025 DOI: 10.2514/6.2025-3273.

  Peer-Reviewed Original Research

• Leading Edge Blowing: A Targeted Approach to Reduce Three Types of Aerofoil Noise

  Bakrania Y, Chong T, Joseph P. Leading Edge Blowing: A Targeted Approach to Reduce Three Types of Aerofoil Noise. 2025 DOI: 10.2514/6.2025-3357.

  Peer-Reviewed Original Research

• Time and Frequency Domain Analysis of Acoustic Pressure From Rotating Forces

  Corbishley T, Joseph P, Paruchuri C. Time and Frequency Domain Analysis of Acoustic Pressure From Rotating Forces. 2025 DOI: 10.2514/6.2025-3498.

  Peer-Reviewed Original Research

• An Iterative Algorithm for the Optimal Control of Propeller Noise Through Synchrophasing

  Joseph P, Paruchuri C, Elliott S, le Duc S, Bhardwaj M, Chong T. An Iterative Algorithm for the Optimal Control of Propeller Noise Through Synchrophasing. 2025 DOI: 10.2514/6.2025-3646.

  Peer-Reviewed Original Research

  Concepts

• Aeroacoustic Investigation of Shrouded Propeller Systems

  Palleja-Cabre S, Ballgjati J, Saraceno I, Joseph P, Paruchuri C, Avallone F. Aeroacoustic Investigation of Shrouded Propeller Systems. 2025 DOI: 10.2514/6.2025-3750.

  Peer-Reviewed Original Research

• On the Aeroacoustic Characterisation of Propellers During Vertical Descent

  Karimian A, Paruchuri C, Joseph P, Liu Y. On the Aeroacoustic Characterisation of Propellers During Vertical Descent. 2025 DOI: 10.2514/6.2025-3755.

  Peer-Reviewed Original Research