Experimental Investigation Of The Effect Of Nose Cavity On The Aerothermodynamics Of The Missile Shaped Bodies Flying At Hypersonic Mach Numbers

Experimental Investigation Of The Effect Of Nose Cavity On The Aerothermodynamics Of The Missile Shaped Bodies Flying At Hypersonic Mach Numbers

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. Introduction of a forward-facing cavity in the nose tip of a blunt body config...

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Bibliographic Details
Main Author: Saravanan, S
Other Authors: Reddy, K P J
Language:en_US
Published: 2010
Subjects:
Hypersonic Aerodynamics
Hypersonic Mach Number
Aerothermodynamics
Hypersonic Flow
Hypersonic Vehicles - Heat Transfer
Flow Visualization
Aerodynamic Heating
Hypersonic Shock Tunnels
Shock Tunnel Testing
Missile Shaped Body
Accelerometer Balance System
Hypersonic Slender Vechicle
Aeronautics
Online Access:http://hdl.handle.net/2005/694

Internet

http://hdl.handle.net/2005/694

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