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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 ...

    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, ...

    Investigation Of Ramp/Cowl Shock Interaction Processes Near A Generic Scramjet Inlet At Hypersonic Mach Number 

    Mahapatra, Debabrata (2010-08-05)
    One of the major technological innovations that are necessary for faster and cheaper access-to-space will be the commercial realization of supersonic combustion jet engines (SCRAMJET). The establishment of the flow through ...

    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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    AuthorMahapatra, Debabrata (1)Ravi, B R (1)Srinath, S (1)Sriram, R (1)Subject
    Aeronautics (4)
    Hypersonic Mach Numbers (4)
    Hypersonic Aerodynamics (3)Drag (Aerodynamics) (2)Hypersonic Flow (2)Hypersonic Mach Number (2)Aerodynamic Heating (1)Aerospike (1)Aerospikes (1)Argon Plasma Jet (1)... View MoreDate Issued2010 (2)2011 (1)2012 (1)Has File(s)Yes (4)

    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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