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    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 ...

    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 ...

    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 ...

    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 ...

    Kinetic Flux Vector Splitting Method On Moving Grids (KFMG) For Unsteady Aerodynamics And Aeroelasticity 

    Krinshnamurthy, R (Indian Institute of Science, 2007-06-07)
    Analysis of unsteady flows is a very challenging topic of research. A decade ago, potential flow equations were used to predict unsteady pressures on oscillating bodies. Recognising the fact that nonlinear aerodynamics is ...

    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 ...

    2D Compressible Viscous Flow Computations Using Acoustic Flux Vector Splitting (AFVS) Scheme 

    Ravikumar, Devaki (Indian Institute of Science, 2007-05-07)
    The present work deals with the extension of Acoustic Flux Vector Splitting (AFVS) scheme for the Compressible Viscous flow computations. Accurate viscous flow computations require much finer grids with adequate clustering ...

    Low Reynolds Number Airfoil Aerodynamics 

    Srinivasa Murthy, P (Indian Institute of Science, 2006-07-21)
    In this thesis we describe the development of Reynolds- averaged Navier Stokes code for the flow past two- dimensional configuration. Particularly, emphasis has been laid on the study of low Reynolds number airfoil ...

    A Methodology To Recover Unstable Aircraft From Post Stall Regimes: Design And Analysis 

    Saraf, Amitabh (Indian Institute of Science, 2006-07-26)
    This thesis deals with high angle of attack behaviour of a generic delta wing model aircraft. A high angle of attack wind tunnel database has been generated for this aircraft and based upon the bifurcation analysis of the ...

    Analysis Of Solar Pumped Chemical Oxygen Iodine Laser 

    Balaji, A (Indian Institute of Science, 2006-10-11)
    Chemical Oxygen Iodine Laser(COIL) is an electronic transition high energy chemical laser having a wavelength of 1.315 /mi. This is the first chemical laser to operate on an electronic rather than a rotational or vibrational ...
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    AuthorAnilkumar, A K (2)Anand Raj, R (1)Anil Kumar, K R (1)Arora, Konark (1)Arora, Rajesh Kumar (1)Ashirvadam, Kampa (1)Balaji, A (1)Bharadwaj, V (1)Bhat, Chandrashekhar (1)C, Praveen (1)... View MoreSubjectAeronautics (14)Aerodynamics (8)Aerospace Engineering (6)Applied Mechanics (5)Astronautics (5)Computational Fluid Dynamics (4)Fluid Dynamics (4)Composite Beam (3)Composite Materials (3)Kalman Filter (3)... View MoreDate Issued2009 (27)2005 (10)2006 (10)2007 (8)Has File(s)Yes (55)

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