Experimental Investigations on Hypersonic Waverider
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 mission requirements. Aerothermodynamics is the basis for designing and develop...
Main Author: | Nagashetty, K |
---|---|
Other Authors: | Reddy, K P J |
Language: | en_US |
Published: |
2018
|
Subjects: | |
Online Access: | http://hdl.handle.net/2005/3195 http://etd.ncsi.iisc.ernet.in/abstracts/4067/G26579-Abs.pdf |
Similar Items
-
Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic aerospace vehicle
by: Tiago Cavalcanti Rolim, et al.
Published: (2011-05-01) -
Experimental Investigation Of The Effect Of Nose Cavity On The Aerothermodynamics Of The Missile Shaped Bodies Flying At Hypersonic Mach Numbers
by: Saravanan, S
Published: (2010) -
Investigation of Heat Transfer Rates Around the Aerodynamic Cavities on a Flat Plate at Hypersonic Mach Numbers
by: Philip, Sarah Jobin
Published: (2018) -
Experimental Study Of Large Angle Blunt Cone With Telescopic Aerospike Flying At Hypersonic Mach Numbers
by: Srinath, S
Published: (2011) -
Shock Tunnel Investigations on Hypersonic Impinging Shock Wave Boundary Layer Interaction
by: Sriram, R
Published: (2018)