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    Browsing Aerospace Engineering (AE) by Title

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    Now showing items 219-238 of 324

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      • Odor Source Localization Using Swarm Robotics 

        Thomas, Joseph (2010-06-02)
        Locating an odor source in a turbulent environment, an instinctive behavior of insects such as moths, is a nontrivial task in robotics. Robots equipped with odor sensors find it difficult to locate the odor source due to the ...
      • On Modeling Of Constrained Piezoelectric Thin Films For Structural Health Monitoring 

        Ali, Rizwaan (2010-01-01)
        The behaviour of a free-standing thin film differs from that of a film surface-bonded or embedded due to the boundary constraints. A general dearth of analytical models, in regard to prediction of the operational competence ...
      • On the Contribution of the Launch Platform towards Acoustic Environment of a Launch Vehicle at Lift-off 

        Karthikeyan, N
        A launch vehicle experiences intense acoustic loading in the initial phase of its lift-off due to the noise generated by the rocket exhaust. This affects the launch vehicle structure in addition to sensitive payloads and ...
      • On The Effect Of Material Uncertainty And Matrix Cracks On Smart Composite Plate 

        Umesh, K (2017-02-22)
        Recent developments show the applications of smart structure in different engineering fields. Smart structures can be used for shape and vibration control, structural health monitoring etc. Smart materials can be integrated ...
      • On The Reduction Of Drag Of a Sphere By Natural Ventilation 

        Suryanarayana, G K (Indian Institute of Science, 2005-07-08)
        The problem of bluff body flows and the drag associated with them has been the subject of numerous investigations in the literature. In the two-dimensional case, the flow past a circular cylinder has been most widely studied ...
      • 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 (2008-04-30)
        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 ...
      • 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 ...
      • 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)
      • Phase Modification And Combustion Studies On Ammonium Nitrate And Propellant Compositions 

        Oommen, Charlie (2012-11-06)
      • 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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