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Experimental investigation of leading edge bluntness on heat transfer rate & flow unsteadiness in shock-induced boundary layer separation in a scramjet intake

Quick Information
Area of Research
Engineering Sciences
Focus Area
Research Sponsored (RESPOND)
Start Year
2020
End Year
2021
Duration
24
Sanction Amount
₹ 27.84 L
Status
Completed
Output
No. of Research Paper
00
Technologies (If Any)
00
No. of PhD Produced
00
No. of Patents
Filed : 00
Grant : 00
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