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    Browsing Aerospace Engineering (AE) by Title

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    Now showing items 54-73 of 324

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      • Decentralized Sustainable Energy Planning For Tumkur District, India 

        Hiremath, Rahul B (2010-02-18)
        The energy-planning involves finding a set of sources and conversion devices so as to meet the energy requirements/demands of all the activities in an optimal manner. This could occur at centralized or decentralized level. ...
      • Decoupled Lateral Directional Flight Control System Design Using Eigenstructure Assignment Method 

        Dixit, Girish G (2012-11-07)
      • Delamination Modeling and Detection in Composite Structures 

        Keshava Kumar, S (2017-12-12)
        Composite laminated structures are prone to delamination. Rotorcraft flexbeams, apart from many other aerospace primary load carrying members are made up of composite laminated structures. A delaminated primary load carrying ...
      • Demonstration Of Supersonic Combustion In A Combustion Driven Shock-Tunnel 

        Joarder, Ratan (2011-01-17)
        For flights beyond Mach 6 ramjets are inefficient engines due to huge total pressure loss in the normal shock systems, combustion conditions that lose a large fraction of the available chemical energy due to dissociation ...
      • 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 ...
      • Design and Development of 75 mm Fixed-Wing Nano Air Vehicle 

        Pushpangathan, Jinraj V (2018-06-11)
        This thesis deals with the design and development of a 75 mm fixed-wing nano-air vehicle (NAV). The NAV is designed to fit inside a cube with each side measuring 75 mm. The range and endurance of the NAV are 300 m and 2-3 ...
      • Design And Development Of Diaphragmless Hypersonic Shock Tunnel 

        Hariharan, M S (2011-03-16)
        The growing requirements to achieve hypersonic flights, as in the case of reentry vehicles, pose a serious challenge to the designers. This demands an understanding of the features of hypersonic flow and its effect on ...
      • 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 ...
      • Design And Evaluation Of Some Stochastic Load Scheduling Algorithms In Distributed Computing Systems 

        Anand, L (2012-01-04)
      • Design of Planar Supersonic Wind Tunnel Nozzle 

        Somani, Dhirendu
        This thesis revisits the design of a planar supersonic nozzle for a supersonic wind tunnel using the method of characteristics (MOC) and Computational Fluid Dynamics (CFD). While design of a converging-diverging (CD) ...
      • A Design Procedure for Flapping Wings Comprising Piezoelectric Actuators, Driver Circuit, and a Compliant Mechanism 

        Chattaraj, Nilanjan (2018-06-05)
        Flapping-wing micro air vehicle (MAV) is an emerging micro-robotic technology, which has several challenges toward its practical implementation. Inspired by insect flight, researchers have adopted bio-mimicking approach ...
      • Design, Development And Flight Control Of Sapthami - A Fixed Wing Micro Air Vehicle 

        Satak, Neha (2010-09-21)
        Two micro air vehicles, namely Sapthami and Sapthami-flyer, are developed in this thesis. Their total weight is less than 200grams each. They fit inside a 30cm and 32cm sphere respectively and carry the commercially available ...
      • Determination Of Isopectral Rotating And Non-Rotating Beams 

        Kambampati, Sandilya (2016-04-27)
        In this work, rotating beams which are isospectral to non-rotating beams are studied. A rotating beam is isospectral to a non-rotating beam if both the beams have the same spectral properties i.e; both the beams have the ...
      • Development and Application of Kinetic Meshless Methods for Euler Equations 

        C, Praveen (Indian Institute of Science, 2005-10-17)
        Meshless methods are a relatively new class of schemes for the numerical solution of partial differential equations. Their special characteristic is that they do not require a mesh but only need a distribution of points ...
      • Development And Design Optimization Of Laminated Composite Structures Using Failure Mechanism Based Failure Criterion 

        Naik, G Narayana (2009-04-27)
        In recent years, use of composites is increasing in most fields of engineering such as aerospace, automotive, civil construction, marine, prosthetics, etc., because of its light weight, very high specific strength and ...
      • Development Of A General Purpose Flow Solver For Euler Equations 

        Shende, Nikhil Vijay (2011-10-14)
      • Development Of A New Finite-Volume Lattice Boltzmann Formulation And Studies On Benchmark Flows 

        Vilasrao, Patil Dhiraj (2011-06-30)
        This thesis is concerned with the new formulation of a finite-volume lattice Boltzmann equation method and its implementation on unstructured meshes. The finite-volume discretization with a cell-centered tessellation is ...
      • Development Of A Plume With Off-Source Volumetric Heating 

        Venkatakrishnan, L (2012-11-07)
      • Development Of Gyroless Attitude And Angular Rate Estimation For Satellites 

        Vivek Chandran, K P (2011-04-06)
        Studies aimed at the development of indigenous low cost star tracker and gyroless attitude and angular rate estimation is presented in the thesis. This study is required for the realization of low cost micro satellites. A ...
      • Development of Novel Heat Transfer Gauges Based on Large Carbon Clusters to Measure Total as well as Radiative Heat Flux for Planetary Entry Configurations in Hypersonic Shock Tunnels 

        Srinath, S
        The quest of travelling beyond earth, preludes with ground based experimental studies, detailed analysis and accurate calculations in the aspects of having a safer design of flying vehicles. As the vehicles plunge into the ...

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