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Experimental Investigation of the Effects of Aerospike Geometry on Aerodynamic Drag and Heat Transfer Rates for a Blunt Body Configuration at Hypersonic Mach Numbers
S SrinathRelated information
1 Department of Aerospace Engineering, Indian Institute of Science, Bangalore-560012, India
, K. P. J ReddyRelated information1 Department of Aerospace Engineering, Indian Institute of Science, Bangalore-560012, India