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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 Investigations on Hypersonic Waverider 

    Nagashetty, K (2018-02-28)
    In the flying field of space transportation domain, the increased efforts involving design and development of hypersonic flight for space missions is on toe to provide the optimum aerothermodynamic design data to satisfy ...

    Experimental Studies on Shock-Shock Interactions in Hypersonic Shock Tunnels 

    Khatta, Abhishek (2017-12-16)
    Shock-shock interactions are among the most basic gas-dynamic problem, and are almost unavoidable in any high speed light, where shock waves generating from different sources crosses each other paths. These interactions ...

    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. ...

    Experimental Analysis of Shock Stand off Distance over Spherical Bodies in Hypersonic Flows 

    Thakur, Ruchi (2018-07-18)
    One of the characteristics of the high speed ows over blunt bodies is the detached shock formed in front of the body. The distance of the shock from the stagnation point measured along the stagnation streamline is termed ...

    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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    AuthorKhatta, Abhishek (1)Kumar, Chintoo Sudhiesh (1)Nagashetty, K (1)Ram, S N (1)Ravi, B R (1)Saravanan, S (1)Satheesh, K (1)Srinath, S (1)Sriram, R (1)Thakur, Ruchi (1)Subject
    Hypersonic Aerodynamics (10)
    Aeronautics (7)Flow Visualization (4)Hypersonic Flow (4)Hypersonic Mach Numbers (4)Hypersonic Shock Tunnels (4)Aerospace Engineering (3)Hypersonic Flows (3)Aerodynamic Heating (2)Aerothermodynamics (2)... View MoreDate Issued2010 (3)2017 (2)2018 (2)2011 (1)2012 (1)2013 (1)Has File(s)Yes (10)

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