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    Linear Instability Of Laterally Strained Constant Pressure Boundary Layer Flows 

    Tyagi, P K (Indian Institute of Science, 2007-03-26)
    The linear instability of laterally diverging/converging flows is an important aspect towards understanding the laminar-transition process in many viscous flows. In this work the linear instability of constant pressure ...

    Experimental And Theoretical Studies On Jet Acoustics 

    Pundarika, G (Indian Institute of Science, 2006-12-14)
    A systematic research on aeroacoustics conducted around the world for the last few decades has revealed various inherent characteristics of the jet noise radiation. However, a lot more needs to be done for the theoretical ...

    Shape Optimization Using A Meshless Flow Solver And Modern Optimization Techniques 

    Sashi Kumar, G N (2009-03-17)
    The development of a shape optimization solver using the existing Computational Fluid Dynamics (CFD) codes is taken up as topic of research in this thesis. A shape optimizer was initially developed based on Genetic ...

    Kinetic Flux Vector Splitting Method On Moving Grids (KFMG) For Unsteady Aerodynamics And Aeroelasticity 

    Krinshnamurthy, R (Indian Institute of Science, 2007-06-07)
    Analysis of unsteady flows is a very challenging topic of research. A decade ago, potential flow equations were used to predict unsteady pressures on oscillating bodies. Recognising the fact that nonlinear aerodynamics is ...

    2D Compressible Viscous Flow Computations Using Acoustic Flux Vector Splitting (AFVS) Scheme 

    Ravikumar, Devaki (Indian Institute of Science, 2007-05-07)
    The present work deals with the extension of Acoustic Flux Vector Splitting (AFVS) scheme for the Compressible Viscous flow computations. Accurate viscous flow computations require much finer grids with adequate clustering ...

    A Numerical Study On Absolute Instability Of Low Density Jets 

    Chakravorty, Saugata (Indian Institute of Science, 2006-07-20)
    A spectacular instability has been observed in low density round jets when the density ratio of jet fluid to ambient fluid falls below a threshold of approximately 0.6. This phenomenon has been observed in non-buoyant jets ...

    Implicit Least Squares Kinetic Upwind Method (LSKUM) And Implicit LSKUM Based On Entropy Variables (q-LSKUM) 

    Swarup, A Sri Sakti (Indian Institute of Science, 2006-10-12)
    With increasing demand for computational solutions of fluid dynamical problems, researchers around the world are working on the development of highly robust numerical schemes capable of solving flow problems around complex ...

    Turbulent Near Wake Behind An Infinitely Yawed Flat Plate 

    Subaschandar, N (Indian Institute of Science, 2005-09-20)
    Near wake is the region of wake flow just behind the trailing edge of the body where the flow is strongly influenced by the upstream flow conditions and also perhaps by the charac­teristics of the body. The present work ...

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    AuthorChakravorty, Saugata (1)Krinshnamurthy, R (1)Pundarika, G (1)Ravikumar, Devaki (1)Sashi Kumar, G N (1)Subaschandar, N (1)Swarup, A Sri Sakti (1)Tyagi, P K (1)Subject
    Aerodynamics (8)
    Air Flow (2)Turbulence (2)Absolute Instability (1)ACO-CFD Method (1)Acoustic Flux Vector Splitting (AFVS) Scheme (1)Acoustic Holography (1)Aerodynamic Shape Optimization (1)Aeroelasticity (1)Aircraft Noise (1)... View MoreDate Issued2006 (3)2007 (3)2005 (1)2009 (1)Has File(s)Yes (8)

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