Application of proper orthogonal decomposition to a supersonic axisymmetric jet

E Caraballo, M Samimy, J Scott, S Narayanan… - AIAA journal, 2003 - arc.aiaa.org
IThasbeenknownfordecadesthatlarge-scalecoherentstructures play a major role in many
engineering applications. Examples include entrainment and mixing in mixers and …

Application of proper orthogonal decomposition to a high speed axisymmetric jet

E Caraballo, M Samimy, S Narayanan… - 15th AIAA …, 2001 - arc.aiaa.org
The work presented here is motivated by an ongoing research program for the use of the
Proper Orthogonal Decomposition (POD) method in conjunction with advanced optical …

Coherent structure in a turbulent jet via a vector implementation of the proper orthogonal decomposition

MO Iqbal, FO Thomas - Journal of Fluid Mechanics, 2007 - cambridge.org
The coherent structure in the near-field of an axisymmetric turbulent jet at a Reynolds
number of 3.8× 105 and Mach number of 0.3 is experimentally characterized by a vector …

A near-field investigation of a supersonic, multi-stream jet: locating turbulence mechanisms through velocity and density measurements

AS Magstadt, MG Berry, TJ Coleman… - 54th AIAA Aerospace …, 2016 - arc.aiaa.org
An experimental investigation into the flow-field of a modern jet nozzle has been carried out.
Even in canonical flows (eg axisymmetric jets), turbulence and its consequences are not …

Analysis of coherent structures in an under-expanded supersonic impinging jet using spectral proper orthogonal decomposition (SPOD)

S Karami, J Soria - Aerospace, 2018 - mdpi.com
The spatiotemporal dynamics of the coherent structures in an under-expanded supersonic
impinging jet are studied using a spectral proper orthogonal decomposition technique. For …

Application of a “slice” proper orthogonal decomposition to the far field of an axisymmetric turbulent jet

S Gamard, WK George, D Jung, S Woodward - Physics of Fluids, 2002 - pubs.aip.org
Earlier experiments on turbulent jets (Crow and Champagne, 1 Brown and Roshko2) made
clear that large structures dominated the physics of the axisymmetric jet. Although no clear …

Three-dimensional spectral pod of supersonic twin-rectangular jet flow

B Yeung, OT Schmidt, GA Brès - AIAA Aviation 2022 Forum, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-3345. vid The statistical analysis of
non-axisymmetric turbulent jets using spectral proper orthogonal decomposition (SPOD) is …

Reduced-order model of a reacting, turbulent supersonic jet based on proper orthogonal decomposition

A Alomar, A Nicole, D Sipp, V Rialland… - … and Computational Fluid …, 2020 - Springer
The present article deals with the spatiotemporal reduction of a reacting, supersonic,
turbulent jet. A flowfield dataset is first obtained from a LES simulation including chemical …

Turbulence and sound-field POD analysis of a turbulent jet

JB Freund, T Colonius - International Journal of …, 2009 - journals.sagepub.com
A Proper Orthogonal Decomposition (POD) is constructed for a Mach 0.9 turbulent jet using
a well-validated direct numerical simulation database. Norms are defined based on near …

Extended proper orthogonal decomposition: Application to jet/vortex interaction

S Maurel1, J Borée1, JL Lumley2 - Flow, Turbulence and Combustion, 2001 - Springer
Abstract The Proper Orthogonal Decomposition (POD) is used in the present work to study
the interactions between different regions of a flow. The standard analysis would select …