C
Charles E. Tinney
Researcher at University of Texas at Austin
Publications - 115
Citations - 2074
Charles E. Tinney is an academic researcher from University of Texas at Austin. The author has contributed to research in topics: Jet (fluid) & Mach number. The author has an hindex of 24, co-authored 104 publications receiving 1802 citations. Previous affiliations of Charles E. Tinney include Centre national de la recherche scientifique & Syracuse University.
Papers
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The near pressure field of co-axial subsonic jets
Charles E. Tinney,Peter Jordan +1 more
TL;DR: In this paper, an analysis of the axial, temporal and azimuthal structure of the pressure field of a co-axial jet with and without serrations on the secondary nozzle lip is presented.
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On spectral linear stochastic estimation
TL;DR: In this article, an extension to classical stochastic estimation techniques is presented, whereby spectral based estimation coefficients are derived from the cross spectral relationship between unconditional and conditional events. But the necessity for this approach stems from instances where the conditional estimates are generated from unconditional sources that do not share the same grid subset, or possess different spectral behaviors than the conditional events, which is essential where accurate modeling using conditional estimation techniques are considered.
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Low-dimensional characteristics of a transonic jet. Part 2. Estimate and far-field prediction
TL;DR: In this article, a low-dimensional and dynamical system model from hydrodynamic pressure signatures was developed for estimating and predicting the behavior of the energy-containing events that govern many of the physical constituents of turbulent flows.
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Low-dimensional characteristics of a transonic jet. Part 1. Proper orthogonal decomposition
TL;DR: In this paper, an experimental investigation concerning the most energetic turbulent features of the flow exiting from an axisymmetric converging nozzle at Mach 0.85 and ambient temperature is discussed using planar optical measurement techniques.
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Multirotor Drone Noise at Static Thrust
Charles E. Tinney,Jayant Sirohi +1 more
TL;DR: In this paper, a first principles understanding of the sound field produced by multi-rotor drones in hover is presented, with configurations ranging from 8 to 12-in. diameters.