• Login
    Search 
    •   etd@IISc
    • Division of Mechanical Sciences
    • Search
    •   etd@IISc
    • Division of Mechanical Sciences
    • Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Search

    Show Advanced FiltersHide Advanced Filters

    Filters

    Use filters to refine the search results.

    Now showing items 1-5 of 5

    • Sort Options:
    • Relevance
    • Title Asc
    • Title Desc
    • Issue Date Asc
    • Issue Date Desc
    • Results Per Page:
    • 5
    • 10
    • 20
    • 40
    • 60
    • 80
    • 100

    Design And Development Of Diaphragmless Hypersonic Shock Tunnel 

    Hariharan, M S (2011-03-16)
    The growing requirements to achieve hypersonic flights, as in the case of reentry vehicles, pose a serious challenge to the designers. This demands an understanding of the features of hypersonic flow and its effect on ...

    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 ...

    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 ...

    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 ...

    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
    Theme by 
    Atmire NV
     

     

    Browse

    All of etd@IIScCommunities & CollectionsTitlesAuthorsAdvisorsSubjectsBy Thesis Submission DateThis CommunityTitlesAuthorsAdvisorsSubjectsBy Thesis Submission Date

    My Account

    LoginRegister

    Discover

    AuthorHariharan, M S (1)Kumar, Chintoo Sudhiesh (1)Ram, S N (1)Reddeppa, P (1)Saravanan, S (1)Subject
    Aeronautics (5)
    Hypersonic Shock Tunnels (5)
    Hypersonic Flow (4)Flow Visualization (3)Hypersonic Aerodynamics (3)Accelerometer Balance System (1)Aerodynamic Heating (1)Aerodynamic Interference Heating (1)Aerothermodynamics (1)Boundary Layer Tripping (1)... View MoreDate Issued2009 (1)2010 (1)2011 (1)2013 (1)2017 (1)Has File(s)
    Yes (5)

    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
    Theme by 
    Atmire NV