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    Experimental Study Of Large Angle Blunt Cone With Telescopic Aerospike Flying At Hypersonic Mach Numbers 

    Srinath, S (2011-04-06)
    The emerging and competitive environment in the space technology requires the improvements in the capability of aerodynamic vehicles. This leads to the analysis in drag reduction of the vehicle along with the minimized ...

    Experimental Investigation Of Aerodynamic Interference Heating Due To Protuberances On Flat Plates And Cones Facing Hypersonic Flows 

    Kumar, Chintoo Sudhiesh (2017-05-24)
    With the age of hypersonic flight imminent just beyond the horizon, researchers are working hard at designing work-arounds for all the major problems as well as the minor quirks associated with it. One such issue, seemingly ...

    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, ...

    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. ...

    Measurement Of Static Pressure Over Bodies In Hypersonic Shock Tunnel Using MEMS-Based Pressure Sensor Array 

    Ram, S N (2013-10-08)
    Hypersonic flow is both fascinating and intriguing mainly because of presence of strong entropy and viscous interactions in the flow field. Notwithstanding the tremendous advancements in numerical modeling in the last ...

    Transpiration Cooling Analysis Including Binary Diffusion Using 2-D Navier-Stokes Equations At Hypersonic Mach Numbers 

    Ravi, B R (2012-11-06)

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    AuthorKumar, Chintoo Sudhiesh (1)Ram, S N (1)Ravi, B R (1)Saravanan, S (1)Satheesh, K (1)Srinath, S (1)Sriram, R (1)Subject
    Aeronautics (7)
    Hypersonic Aerodynamics (7)
    Hypersonic Flow (4)Flow Visualization (3)Hypersonic Mach Numbers (3)Hypersonic Shock Tunnels (3)Aerodynamic Heating (2)Drag (Aerodynamics) (2)Hypersonic Mach Number (2)Accelerometer Balance System (1)... View MoreDate Issued2010 (3)2011 (1)2012 (1)2013 (1)2017 (1)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
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