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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, ...

    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. ...

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    AuthorSaravanan, S (1)Sriram, R (1)Subject
    Aeronautics (2)
    Flow Visualization (2)
    Hypersonic Aerodynamics (2)
    Hypersonic Flow (2)
    Hypersonic Mach Number (2)Accelerometer Balance System (1)Aerodynamic Heating (1)Aerospikes (1)Aerothermodynamics (1)Counter-flow Injectuon (1)... View MoreDate Issued2010 (2)Has File(s)Yes (2)

    etd@IISc is a joint service of SERC & J R D Tata Memorial (JRDTML) Library || Powered by DSpace software || DuraSpace
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