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    Experimental Investigations on Hypersonic Waverider 

    Nagashetty, K (2018-02-28)
    In the flying field of space transportation domain, the increased efforts involving design and development of hypersonic flight for space missions is on toe to provide the optimum aerothermodynamic design data to satisfy ...

    Effective Property Estimation of Carbon Composites using Micromechanical Modeling 

    Aswathi, S (2018-02-28)
    In recent times, composite materials have gained mainstay acceptance as a structural material of choice due to their tailorability and improved thermal, specific strength/stiffness and durability performance. Carbon-Carbon ...

    Shock Tunnel Investigations on Hypersonic Impinging Shock Wave Boundary Layer Interaction 

    Sriram, R (2018-04-13)
    The interaction of a shock wave and boundary layer often occurs in high speed flows. For sufficiently strong shock strengths the boundary layer separates, generating shock patterns in the contiguous inviscid flow (termed ...

    Vision-based Strategies for Landing of Fixed Wing Unmanned Aerial Vehicles 

    Marianandam, Peter Arun (2018-05-14)
    Vision-based conventional landing of a fixed wing UAV is addressed in this thesis. The work includes mathematical modeling, interface to a software for rendering the outside scenery, image processing techniques, control law ...

    Hybird Central Solvers for Hyperbolic Conservation Laws 

    Maruthi, N H (2018-05-11)
    The hyperbolic conservation laws model the phenomena of nonlinear waves including discontinuities. The coupled nonlinear equations representing such conservation laws may lead to discontinuous solutions even for smooth ...

    A Ghost Fluid Method for Modelling Liquid Jet Atomization 

    Kiran, S (2018-05-21)
    Liquid jet atomisation has a wide variety of application in areas such as injectors in automobile and launch vehicle combustors, spray painting, ink jet printing etc. Understanding physical mechanisms involved in the primary ...

    Analysis of Unsteady Incompressible Potential Flow Over a Swimming Slender Fish and a Swept Wing Tail 

    Nathan, Vinay (2018-05-16)
    This thesis deals with computing the pressure distribution around a swimming slender fish and the thrust generated by its flapping motion. The body of the fish is modeled as a missile like slender body to which a tail is ...

    Analysis of Thick Laminated Composite Beams using Variational Asymptotic Method 

    Ameen, Maqsood Mohammed (2018-06-18)
    An asymptotically-exact methodology is presented for obtaining the cross-sectional stiffness matrix of a pre-twisted, moderately-thick beam having rectangular cross sections and made of transversely isotropic material. The ...

    Modeling of Contact in Orthotropic Materials using Variational Asymptotic Method 

    Eswaran, Jai Kiran (2018-06-18)
    Composites are materials which cater to the present and future needs of many demanding industries, such as aerospace, as they are weight-sensitive for a given requirement of strength and stiff ness, corrosion resistant, ...

    Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction 

    Mallick, Rajnish (2018-01-09)
    This research investigates on-blade partial span active plain trailing edge flaps (TEFs)with an aim to alleviate the helicopter vibrations. Among all the available smart materials, piezoelectric stack actuator(PEA)has shown ...
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    AuthorAnilkumar, A K (2)Sarkar, Korak (2)Aatresh, K (1)Abdul Saleem, P K (1)Akhil, G (1)Allamaprabhu, Yaravintelimath (1)Ameen, Maqsood Mohammed (1)Anil Kumar, K R (1)Aswathi, S (1)Bardhan, Rajarshi (1)... View MoreSubject
    Aerospace Engineering (95)
    Aerodynamics (7)Hypersonic Flows (5)Computational Fluid Dynamics (4)Flow Visualization (4)Fluid Dynamics (3)Fluid Mechanics (3)Guidance Laws (3)Hypersonic Aerodynamics (3)Hypersonic Mach Numbers (3)... View MoreDate Issued2010 - 2018 (71)2005 - 2009 (6)Has File(s)Yes (95)

    etd@IISc is a joint service of SERC & J R D Tata Memorial (JRDTML) Library || Powered by DSpace software || DuraSpace
    Contact Us | Send Feedback | Thesis Templates
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