P

PD Moore

16 records found

An advection-based model to increase the temporal resolution of PIV time series

Two techniques for PIV based aerocaustic prediction and their to a rod-airfoil experiment

An advection-based model to incease the temporal resolution of PIV time-series

Two techniques for PIV-based aeroacoustic prediction and their application to a rod-airfoil experiment

High speed PIV applied to aerodynamic noise investigation
Journal article (2010) - V Koschatzky (author), PD Moore (author), PD Moore (author), Jerry Westerweel (author), J Westerweel (author), J. Westerweel (author), Fulvio Scarano (author), F Scarano (author), F. Scarano (author), B.J. Jan Boersma (author), B.J. Jan Boersma (author), Bendiks Jan Boersma (author), Bendiks Jan Boersma (author), B. J. Boersma (author), B. J. Boersma (author), Bendiks J. Jan Boersma (author), Bendiks J. Jan Boersma (author), BJ Boersma (author), BJ Boersma (author), B.J. Boersma (author), B.J. Boersma (author), Bendiks Jan Boersma (author), Bendiks Jan Boersma (author), BJ Jan Boersma (author), BJ Jan Boersma (author), Bendiks Boersma (author), Bendiks Boersma (author), Bendiks J. Boersma (author), Bendiks J. Boersma (author), B. J. Jan Boersma (author), B. J. Jan Boersma (author), Bendiks Jan Jan Boersma (author), Bendiks Jan Jan Boersma (author)

On the Suitability of Direct Application of Acoustic Theroy to Time-Resolved Tomographic PIV Tested by DNS for Low Mach Number Jet Flows

Application of Powell's analogy for the prediction of vortex-pairing sound in a low-Mach number jet based on time-resolved planar and tomographic PIV

Lagrangian and Eulerian pressure field evaluation of rod-airfoil flow from time-resolved tomographic PIV

An advection model to increase the time-resolution of PIV time-series

Rod-airfoil flow investigation by time-resolved TOMO PIV for aeroacoustics

Aeroacoustics of compressible subsonic jets

Comparison of two techniques for aeroacoustic determination from a rod-airfoil PIV experiment

Aeroacoustic analysis of a rod-airfoil flow by means of time-resolved PIV

Experiments on the flow field and acoustic properties of a Mach number 0.75 turbulent air jet at a low Reynolds number
Journal article (2009) - HJ Slot (author), HJ Slot (author), PD Moore (author), PD Moore (author), R. Delfos (author), R Delfos (author), Rene Delfos (author), René Delfos (author), Bendiks Boersma (author), Bendiks Boersma (author), B. J. Jan Boersma (author), B. J. Jan Boersma (author), B.J. Jan Boersma (author), B.J. Jan Boersma (author), Bendiks J. Boersma (author), Bendiks J. Boersma (author), B. J. Boersma (author), B. J. Boersma (author), Bendiks Jan Boersma (author), Bendiks Jan Boersma (author), Bendiks J. Jan Boersma (author), Bendiks J. Jan Boersma (author), BJ Boersma (author), BJ Boersma (author), BJ Jan Boersma (author), BJ Jan Boersma (author), B.J. Boersma (author), B.J. Boersma (author), Bendiks Jan Boersma (author), Bendiks Jan Boersma (author), Bendiks Jan Jan Boersma (author), Bendiks Jan Jan Boersma (author)

Simulation and measurement of flow generated noise

Use of surface integral methods in the computation of the acoustic far field of a turbulent jet