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    Aeroelasticity of Flapping Wings towards Micro Air Vehicle Applications 

    Mukherjee, Indrajit
    Studies have revealed that insect like flapping flight can serve as a benchmark in designing Micro Aerial Vehicles (MAV) owing to its power efficiency and high maneuverability. Primarily envisioned as agents facilitating ...

    Design and Analysis of Multifunctional Composites for Unmanned Aerial Vehicles 

    Rammohan, B
    The principal aim of this thesis is to analyse the effectiveness of multifunctional composites as intelligent structures to improve mechanical properties and activate additional non-structural features. In order to investigate ...

    Discrete Velocity Boltzmann Schemes for Inviscid Compressible Flows 

    Raghavendra, Nandagiri Venkata
    It is known that high-speed flows are compressible. In large parts of the flow domains, the inviscid approximation is valid and this leads to Euler equations of gas dynamics. These inviscid compressible flows are modelled ...

    Ionic Polymer Metal Composite Actuators for Insect Scale Flapping Wing Micro Air Vehicle 

    Swarrup, J Sakthi
    Flapping wing micro air vehicles (MAV) have broad applications such as exploration in hazardous environment, reconnaissance, search and rescue. Ionic polymer metal composites (IPMC) have emerged as a promising material ...

    Flutter Identification and Aeroelastic Stability during Wake Penetration 

    Sudha, U P V
    Demonstration of utter stability over the design envelope and identi fication of safe ight envelope is a prerequisite for operational clearance of any new aircraft design. An important step involved in flight flutter ...

    The Role of Self-Recirculating Casing Treatment on Axial Compressor and Its Aeroelastic Behavior 

    Kumar, S Satish
    The modern-day axial compressor stages in a gas turbine engine play a vital role in generating the high-pressure ratios by operating at the limits of their design. Aerodynamic instabilities such as rotating stall and surge ...

    Constrained Adaptive Control of Nonlinear Systems with Application to Hypersonic Vehicles 

    Sachan, Kapil
    Constraints in input, output, and states are evident in most of the practical systems. Explicitly incorporating these constraints into the control design process leads to its superior performance in general. Therefore, ...

    Analysis of Kinematic Constraints in Fixed-Wing UAV Formation Flying 

    Challa, Vinay Reddy
    Rise in autonomy has led to increase in usage of Unmanned Aerial Vehicles (UAVs) for various applications and has allowed the UAVs to perform complex and hazardous missions with ease. Formation of multiple UAVs finds ...

    Mechanical Characterization of Carbon Nanotubes and Nanocomposites 

    Jalan, Salil Kanj (2018-08-14)
    Measurement of all the mechanical properties of carbon nanotubes is extremely difficult because of its small size. In the present work, all the five transverse isotropic properties of single wall carbon nanotubes (SWCNTs) ...

    Experimental and Theoretical Studies of Liquid Drop Impact on Solid Surfaces Comprising Smooth and Texture Portions 

    Vaikuntanathan, Visakh (2018-08-10)
    Solid surfaces featuring a spatial variation of surface wettability along particular directions on their surface, referred to as wettability gradient surfaces, are becoming increasingly important in practical applications ...
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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)

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