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    Now showing items 292-311 of 424

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      • On the Structure and Propagation of Premixed Flames in Turbulence 

        Dave, Himanshu L
        Turbulence interacts with flames over a multitude of lengthscales and timescales. These interactions are nonlinear and are ubiquitous, for example, in propulsion engines operating in space, air, land, and sea. ...
      • On Three Dimensional High Lift Flow Computations 

        Gopalakrishna, N (2018-02-18)
        Computing 3D high lift flows has been a challenge to the CFD community because of three important reasons: complex physics, complex geometries and large computational requirements. In the recent years, considerable progress ...
      • On Viscous Flux Discretization Procedures For Finite Volume And Meshless Solvers 

        Munikrishna, N (2009-04-29)
        This work deals with discretizing viscous fluxes in the context of unstructured data based finite volume and meshless solvers, two competing methodologies for simulating viscous flows past complex industrial geometries. ...
      • Onboard Propellant Gauging For Spacecraft 

        Lal, Amit (2009-08-04)
        Estimation of the total mission life of a spacecraft is an important issue for the communication satellite industries. For accurate determination of the remaining mission life of the satellite it is essential to estimate ...
      • Optimal Control Of Numerical Dissipation In Modified KFVS (m-KFVS) Using Discrete Adjoint Method 

        Anil, N (2010-06-04)
        The kinetic schemes, also known as Boltzmann schemes are based on the moment-method-strategy, where an upwind scheme is first developed at the Boltzmann level and after taking suitable moments we arrive at an upwind scheme ...
      • Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines 

        Maity, Arnab (2016-07-11)
        A new suboptimal guidance law design approach for aerospace vehicles is proposed in this thesis, followed by an advanced control design for supersonic air-breathing engines. The guidance law is designed using the newly ...
      • Optimal Numerical Integration Method for Higher Order Polygonal Finite Elements and its application in microstructure modeling 

        Kunjam, Prashant
        In conventional Finite Element Method (FEM), triangular and quadrilateral elements are commonly used finite elements and their counterparts with tetrahedral and hexahedral elements in three-dimensions to discretize the ...
      • Optimal Resource Allocation In Lanchester Attrition Model Based Conflicts 

        Sheeba, P S (2009-05-06)
        Force deployment and optimal resource allocation has been an area of considerable research interest in conventional warfare. In the modern scenario, with significant advances in technology related to communication and ...
      • Optimal Trajectory Planning for Fixed-Wing Miniature Air Vehicles 

        Hota, Sikha (2018-04-02)
        Applications such as urban surveillance, search and rescue, agricultural applications, military applications, etc., require miniature air vehicles (MAVs) to fly for a long time. But they have restricted flight duration due ...
      • Optimization of a higher-order sandwich composite beam under uncertainties 

        Sharma, Himanshu
        Optimization under uncertainties of structures is a challenging field due to the requirements of high computational resources. The typical approaches include reliability-based design optimization (RBDO) and robust design ...
      • Packed Bed Gasification-Combustion In Biomass Based Domestic Stoves And Combustion Systems 

        Varunkumar, S (2014-07-04)
        This thesis constitutes fundamental experimental and computational investigations on gasification and combustion in a packed bed of biomass. Packed bed gasification-combustion in counter-current mode is used in two ...
      • Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source 

        Bhaskaran, Ramprasad (2014-07-11)
        Stirling engines are promising candidates for applications where air breathing engines cannot be used. Self contained engines capable of operating independently of the environment are required to convert thermal energy ...
      • Particle Image Velocimetry (PIV) Measurements In A Low Intermittency Transitional Flow 

        Mandal, Alakesh Chandra (2011-10-12)
      • Passive control and intermittent dynamics of the precessing vortex core oscillation in swirl flows 

        Gupta, Saarthak
        Swirl is used in modern gas turbine combustor nozzles to achieve reliable flame stabilization and efficient fuel-air mixing. The swirl component in the nozzle jet flow induces an axial vortex. At high swirl intensities, ...
      • Permeability Modeling for Single Scale and Dual Scale Fabrics and its implementation to Fabrics Undergoing Shear 

        Godbole, Mayur G
        Composites have found applications, right from high-end aerospace structures to naval and land-based structures. These structures are realized by manufacturing processes like, autoclave and vacuum assisted resin transfer ...
      • Phase Modification And Combustion Studies On Ammonium Nitrate And Propellant Compositions 

        Oommen, Charlie (2012-11-06)
      • Phononic bandgap engineering in cellular periodic structures and mechanical metamaterials 

        Mukherjee, Sushovan
        A methodology has been developed for the computation of phononic band structure of cellular periodic structures, structures with spatially repetitive patterns, using Frequency domain Spectral Finite Element Method along ...
      • Physical insights into unstart dynamics of a hypersonic mixed compression intake 

        Devaraj, Manoj Kumar K
        Hypersonic air-breathing cruise vehicles powered by supersonic combustion ramjet engines are the potential candidate for future space and defense applications. The air intake of the scramjet engine is a vital component ...
      • Piezoceramic Dynamic Hysteresis Effects On Helicopter Vibration Control Using Multiple Trailing-Edge Flaps 

        Viswamurthy, S R (2009-07-14)
        Helicopters suffer from severe vibration levels compared to fixed-wing aircraft. The main source of vibration in a helicopter is the main rotor which operates in a highly unsteady aerodynamic environment. Active vibration ...
      • Plasmon Phonon Coupled Dynamics of Nanocrystalline Structures 

        Javvaji, Brahmanandam
        This thesis is an attempt to understand the characteristics and responses of plasmon phonon coupled dynamics in nanocrystalline structures. An energy based Lagrangian formulation is developed with fundamental field quantities ...

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