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    Browsing Aerospace Engineering (AE) by Title

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    Now showing items 390-409 of 425

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      • Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion 

        Parthiban, S (2012-01-03)
      • Thermal Behaviour Of Mono-Fibre Composites And Hybrid Composites At Cryogenic Temperatures 

        Praveen, R S (2013-01-31)
        Hybrid composites forms an important field of research in the area of composite science and engineering as it gives the advantage of avoiding complex lay-up designs and provides better tuning compatibility to get desired ...
      • Three Dimensional Computational Fluid Dynamic Simulation and Analysis of a Turbocharger Compressor 

        Sharma, Ashutosh (2018-05-01)
        This thesis constitutes detailed computational investigation on ow through the passages of a centrifugal compressor used for turbocharging applications. Given the dynamic nature of operation of the turbocharger, it becomes ...
      • Time Domain Spectral Finite Element Simulation of Ultrasonic Wave Propagation in Composite with Defects 

        Munian, Rajendra Kumar
        Ultrasonic guided wave-based detection of structural defects or damages is one of the promising methods for structural health monitoring (SHM). A significant proportion of structural elements in an aircraft structure and ...
      • Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors 

        Das, Priya G (2011-03-17)
        To address the concern of classical guidance and control designs (where guidance and control loops are designed separately in an “outer loop – inner loop” structure), integrated guidance and control (IGC) ideas have been ...
      • Time-Optimal Guidance for Impact Angle Constrained Interception of Moving Targets 

        Akhil, G (2018-05-30)
        Various unmanned missions deploy vehicles such as missiles, torpedoes, ground robots, and unmanned aerial vehicles. Guidance strategies for these vehicles aim to intercept a target point and satisfy additional objectives ...
      • Transition Zone In Constant Pressure Boundary Layer With Converging Streamlines 

        Vasudevan, K P (Indian Institute of Science, 2007-04-18)
        The laminar-turbulent transition in viscous fluid flows is one of the most intriguing problems in fluid dynamics today. In view of the enormous applications it has in a variety of fields such as aircraft design, turbomachinery, ...
      • Transonic Shock Buffet in an Axial Flow Fan 

        Majhi, Jyoti Ranjan
        Transonic shock buffet, a self-sustained shock oscillation resulting from shock-boundary layer interaction, is observed across a range of operating points on the performance map of a transonic axial flow fan. Shock ...
      • Transpiration Cooling Analysis Including Binary Diffusion Using 2-D Navier-Stokes Equations At Hypersonic Mach Numbers 

        Ravi, B R (2012-11-06)
      • Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles 

        Allamaprabhu, Yaravintelimath (2018-01-30)
        Convergent-Divergent (C-D) nozzles are used in rocket engines to produce thrust as a reaction to the acceleration of hot combustion chamber gases in the opposite direction. To maximize the engine performance at high ...
      • Turbulence-Premixed Flame Interactions 

        Abinesh, M
        The interaction between premixed flames and turbulence is an inherently non-linear phenomenon. Understanding such interactions has profound practical implications towards the development of better combustion devices and ...
      • Turbulent Jet Diffusion Flame : Studies On Lliftoff, Stabilization And Autoignition 

        Patwardhan, Saurabh Sudhir (2010-07-09)
        This thesis is concerned with investigations on two related issues of turbulent jet diffusion flame, namely (a) stabilization at liftoff and (b) autoignition in a turbulent jet diffusion flame. The approach of Conditional ...
      • 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 ...
      • Two Problems on the Parametric Resonances and Bifurcations in Rotating Beams 

        Gagan, Versha
        The current research work addresses two interesting systems related to rotating beams. The first dynamical system under consideration is an articulated uniform beam rotating in vacuum under vertical hub excitation along ...
      • UAV Group Autonomy In Network Centric Environment 

        Suresh, M (2016-11-23)
        It is a well-recognized fact that unmanned aerial vehicles are an essential element in today’s network-centric integrated battlefield environment. Compared to solo UAV missions, multiple unmanned aerial vehicles deployed ...
      • Ultra High Compression For Weather Radar Reflectivity Data 

        Makkapati, Vishnu Vardhan (2007-10-09)
        Weather is a major contributing factor in aviation accidents, incidents and delays. Doppler weather radar has emerged as a potent tool to observe weather. Aircraft carry onboard radars but their range and angular resolution ...
      • Ultrasonic Guided Wave Based Models, Devices and Methods for Integrated Structural Health Monitoring 

        Rathod, Vivek T (2018-01-31)
        Structural Health Monitoring (SHM) systems for future structures and vehicles would involve a process of damage identification and prediction of certain quantities of interest that concerns the function and safety. This ...
      • Ultrasonic Guided Wave-based Inspection of Additively Manufactured Components 

        Dube, Anoop Kumar
        Layered structural components, such as laminated composites and those made via Additive Manufacturing (AM), are widely used in aerospace and automotive industries due to their various advantages. The layer-wise approach ...
      • Uncertainty modeling and analysis of aerospace structures 

        Mukherjee, Shuvajit
        Aerospace structures are different from other structures due to the difference in the required properties for an aerospace application. The primary motivation of this kind of structure lies in its lightweight nature, ...
      • Understanding High Speed Mixing Layers with LES and Evolution of Urans Modeling 

        Sundaram, Iyer Arvind (2017-11-15)
        This thesis is concerned with studies on spatially developing high speed mixing layers with twin objectives: (a) to provide enhanced and detailed understanding of spatial development of two-dimensional mixing layer emanating ...

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