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    •   etd@IISc
    • Division of Mechanical Sciences
    • Aerospace Engineering (AE)
    • Browsing Aerospace Engineering (AE) by thesis submitted date
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    Browsing Aerospace Engineering (AE) by thesis submitted date"2007"

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      • Aerodynamic Analysis Of Grid Fins Using Analytical And Computational Methods 

        Theerthamalai, P (2009-07-16)
        Grid fins (lattice fins) are used as a lifting and control surface for highly manoeuvrable missiles. Grid fins also find their applications for air-launched submunitions. The main advantages are its low hinge moment ...
      • Analysis Of Coupled-Resonator Slow-Wave Structures For Traveling-Wave Tubes For Aerospace Applications 

        Christie, V Latha (2009-04-30)
        Through continued innovation and growth, traveling wave tube amplifiers (TWTAs) remains the microwave power amplifiers of choice in a wide range of high power microwave and millimeter-wave applications specifically for ...
      • An Anti-Skid Brake Controller For A Fighter Aircraft With An Elastic Strut 

        Kumar, V V Nagendra (2009-04-29)
        This thesis deals with the design of an anti-skid brake controller for a generic fighter aircraft. Antiskid brake controllers prevent wheel locking and maximize the coefficient of friction between the tyre and the ground, ...
      • Co-operative Destabilization of a Flat Plate Boundary Layer by a Free Stream Convecting Vortex and Wall Suction/Blowing 

        Vinod Kumar, B G
        The stability of wall bounded shear layer at subcritical Reynolds number disturbed by a freestream convecting vortex and unsteady suction/blowing at the wall was studied. A counterclockwise line vortex was convected parallel ...
      • Combustion Instability Screech In Gas Turbine Afterburner 

        Ashirvadam, Kampa (2009-08-04)
        Gas turbine reheat thrust augmenters known as afterburners are used to provide additional thrust during emergencies, take off, combat, and in supersonic flight of high-performance aircrafts. During the course of reheat ...
      • The Effect Of Energy Deposition In Hypersonic Blunt Body Flow Field 

        Satheesh, K (2010-09-23)
        A body exposed to hypersonic flow is subjected to extremely high wall heating rates, owing to the conversion of the kinetic energy of the oncoming flow into heat through the formation of shock waves and viscous dissipation ...
      • Experimental Investigation Of The Effect Of Nose Cavity On The Aerothermodynamics Of The Missile Shaped Bodies Flying At Hypersonic Mach Numbers 

        Saravanan, S (2010-06-01)
        Hypersonic vehicles are exposed to severe heating loads during their flight in the atmosphere. In order to minimize the heating problem, a variety of cooling techniques are presently available for hypersonic blunt bodies. ...
      • Experimental Investigations Of Surface Interactions Of Shock Heated Gases On High Temperature Materials Using High Enthalpy Shock Tubes 

        Jayaram, V (2009-05-12)
        The re-entry space vehicles encounter high temperatures when they enter the earth atmosphere and the high temperature air in the shock layer around the body undergoes partial dissociation. Also, the gas molecules injected ...
      • Glowworm Swarm Optimization : A Multimodal Function Optimization Paradigm With Applications To Multiple Signal Source Localization Tasks 

        Krishnanand, K N (2009-05-05)
        Multimodal function optimization generally focuses on algorithms to find either a local optimum or the global optimum while avoiding local optima. However, there is another class of optimization problems which have the ...
      • Mode-3 Asymptotic Analysis Around A Crack Embedded In A Ductile Functionally Graded Material 

        Chandar, B Bhanu (2009-09-15)
        Functionally graded materials (FGMs) are composites with continuous material property variations. The distinct interfaces between the reinforcement and the matrix in classical composites are potential damage initiation ...
      • Multi-agent Consensus Using Generalized Cyclic Pursuit Strategies 

        Sinha, Arpita (2009-05-11)
        One of the main focus of research on multi-agent systems is that of coordination in a group of agents to solve problems that are beyond the capability of a single agent. Each agent in the multi-agent system has limited ...
      • A Neural Network Approach To Rotorcraft Parameter Estimation 

        Kumar, Rajan (2009-07-03)
        The present work focuses on the system identification method of aerodynamic parameter estimation which is used to calculate the stability and control derivatives required for aircraft flight mechanics. A new rotorcraft ...
      • 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 (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 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 ...
      • 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 ...
      • Shock Tunnel Investigations On Hypersonic Separated Flows 

        Reddeppa, P (2009-08-11)
        Knowledge of flow separation is very essential for proper understanding of both external and internal aerothermodynamics of bodies. Because of unique flow features such as thick boundary layers, merged shock layers, strong ...
      • Structural Health Monitoring Of Composite Structures Using Magnetostrictive Sensors And Actuators 

        Ghosh, Debiprasad (2009-07-14)
        Fiber reinforced composite materials are widely used in aerospace, mechanical, civil and other industries because of their high strength-to-weight and stiffness-to-weight ratios. However, composite structures are highly ...
      • Studies On Impinging-Jet Atomizers 

        Gadgil, Hrishikesh Prabhakar (2009-05-06)
        Characteristics of impinging-jet atomizers in the context of application in liquid propulsion systems are studied in this thesis. A review of past studies on impinging jets revealed the necessity of a correlation in terms ...
      • Super-Convergent Finite Elements For Analysis Of Higher Order Laminated Composite Beams 

        Murthy, MVVS (2009-08-12)
        Advances in the design and manufacturing technologies have greatly enhanced the utility of fiber reinforced composite materials in aircraft, helicopter and space- craft structural components. The special characteristics ...

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