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    Investigations On Film Cooling At Hypersonic Mach Number Using Forward Facing Injection From Micro-Jet Array 

    Sriram, R (2010-07-16)
    A body in a hypersonic flow field will experience very high heating especially during re-entry. Conventionally this problem is tackled to some extent by the use of large angle blunt cones. At the cost of increased drag, ...

    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 ...

    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 ...

    Computational And Experimental Studies On Flameless Combustion Of Gaseous Fuels 

    Sudarshan Kumar, * (2011-04-13)

    Study Of Aerodynamic Effectiveness Of Wing Tip Sails For Gust Load Alleviation 

    Agarwal, R K (2011-04-29)

    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 ...

    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 ...

    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 ...
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    AuthorMandal, Alakesh Chandra (2)Agarwal, R K (1)Ajit, Dixit Shivsai (1)Anil, N (1)Arjun, B S (1)Behera, Upendra (1)Bodi, Kowsik V R (1)Chakraborty, Debasis (1)Chandar, B Bhanu (1)Chandra Sekhar, D (1)... View MoreSubject
    Aeronautics (85)
    Aerodynamics (14)Hypersonic Flow (8)Hypersonic Aerodynamics (7)Helicopter Rotor Blades (6)Flow Visualization (5)Hypersonic Shock Tunnels (5)Aeroelastic Analysis (4)Computational Fluid Dynamics (4)Hypersonic Mach Numbers (4)... View MoreDate Issued2010 - 2018 (71)2005 - 2009 (14)Has File(s)
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    etd@IISc is a joint service of SERC & J R D Tata Memorial (JRDTML) Library || Powered by DSpace software || DuraSpace
    Contact Us | Send Feedback | Thesis Templates
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