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Preliminary aerodynamic predictions in highly loaded S-shaped ducts by viscous-inviscid interaction
Preliminary aerodynamic predictions in highly loaded S-shaped ducts by viscous-inviscid interaction
Funding
EPSRC CDT in Gas Turbine Aerodynamics
History
School
- Aeronautical, Automotive, Chemical and Materials Engineering
Department
- Aeronautical and Automotive Engineering
Publisher
Loughborough UniversityRights holder
© A. VeyratPublication date
2022Notes
A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of the degree of Doctor of Philosophy of Loughborough University.Language
enSupervisor(s)
A. D. Walker ; J. F. CarrotteQualification name
PhDQualification level
DoctoralThis submission includes a signed certificate in addition to the thesis file(s)
I have submitted a signed certificateAdministrator link
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Categories
Keywords
turbomachinery methodsduct toolboxpreliminary designrapid aerodynamic analysiscurved flowperformance estimateDESIGN SPACE EXPLORATIONchain of cubic parametric splinecentripetal Catmull-Rom splineBezier splineannulus modellercross-sectionradial strutstrutted ductsingly curvilinear orthogonal coordinate systemPotential Theorythree-point parametric methodradial equilibriumthroughflowcentripetal forces equationstreamline curvaturestreamline reconstructionquasi-three-dimensional coreequivalent inviscid flow fieldsuperimposition techniqueboundary layer theoryfairly thin shear layer theoryBoundary Layer Separationnon-equilibrium turbulent shear layermomentum integral equationshape factor equationentrainmententrainment/maximum shear stress correlationcomposite law-of-the-wallmixing length theorybuoyancy/curvature analogyturbulence calibrationSkin friction coefficientstatic pressure coefficientsmoothingdirect couplingiterative schemeGaussian process regressionordinary krigingevenly spaced samplescomposite databasevariance incrementDelaunay Triangulation
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