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    • 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"2006"

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    Now showing items 1-11 of 11

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      • 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 ...
      • Improved Solution Techniques For Trajectory Optimization With Application To A RLV-Demonstrator Mission 

        Arora, Rajesh Kumar (2009-03-12)
        Solutions to trajectory optimization problems are carried out by the direct and indirect methods. Under broad heading of these methods, numerous algorithms such as collocation, direct, indirect and multiple shooting methods ...
      • An Investigation of Architectures For Integration Of Stand-Alone INS And GPS Navigation Systems 

        Dikshit, Veena G (2009-07-08)
        Inertial navigation systems (INSs) have the well-known advantages of being self-contained, weatherproof, jam-proof, and non-self-revealing while providing stable navigation information with little high-frequency noise. ...
      • Kalman Filter Estimation Of Ionospheric TEC And Differential Instrumental Biases Over Low Latitude Using Dual Frequency GPS Observations 

        Anand Raj, R (2009-03-13)
        The low latitude tropical ionosphere has been investigated by various researchers using Global Positioning System (GPS). Presently for many civil aviation applications, the ionospheric modeling of the tropical region has ...
      • Numerical Simulations Of Axisymmetric Near Wakes At High Reynolds Numbers 

        Devi, Ravindra G (2009-03-13)
        The flow past the needle of a Pelton turbine injector is an axisymmetric wake embedded in a round jet. The wake does not fully relax to yield a uniform velocity jet due to the short distance between ...
      • Rotationally Invariant Kinetic Upwind Method (KUMARI) 

        Malagi, Keshav Shrinivas (2009-03-11)
        In the quest for a high fidelity numerical scheme for CFD it is necessary to satisfy demands on accuracy, conservation, positivity and upwinding. Recently the requirement of rotational invariance has been added to this ...
      • Shape Optimization Using A Meshless Flow Solver And Modern Optimization Techniques 

        Sashi Kumar, G N (2009-03-17)
        The development of a shape optimization solver using the existing Computational Fluid Dynamics (CFD) codes is taken up as topic of research in this thesis. A shape optimizer was initially developed based on Genetic ...
      • Structural Health Monitoring Of Composite Helicopter Rotor Blades 

        Pawar, Prashant M (Indian Institute of Science, 2007-04-18)
        Helicopter rotor system operates in a highly dynamic and unsteady aerodynamic environment leading to severe vibratory loads on the rotor system. Repeated exposure to these severe loading conditions can induce damage in the ...
      • 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 ...
      • Wavelet Based Spectral Finite Elements For Wave Propagation Analysis In Isotropic, Composite And Nano-Composite Structures 

        Mitra, Mira (2009-04-02)
        Wave propagation is a common phenomenon in aircraft structures resulting from high velocity transient loadings like bird hit, gust etc. Apart from understanding the behavior of structures under such loading, wave propagation ...
      • Weighted Least Squares Kinetic Upwind Method Using Eigendirections (WLSKUM-ED) 

        Arora, Konark (2009-06-24)
        Least Squares Kinetic Upwind Method (LSKUM), a grid free method based on kinetic schemes has been gaining popularity over the conventional CFD methods for computation of inviscid and viscous compressible flows past complex ...

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