Multi-walled carbon nano-tubes for performance enhancement of thin film heat flux sensors

Author:

Jadhav Akash,Peetala Ravi,Kulkarni Vinayak

Funder

Science and Engineering Research Board

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,Condensed Matter Physics

Reference46 articles.

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2. Vidal RJ (1956) Model instrumentation techniques for heat transfer and force measurements in a hypersonic shock tunnel. Cornell Aeronautical Laboratory, Report No WADC TN 56-315

3. Kulkarni V, Hegde GM, Jagadeesh G, Arunan E, Reddy KPJ (2008) Aerodynamic drag reduction by heat addition into the shock layer for a large angle blunt cone in hypersonic flow. Phys Fluids 20(8):081703

4. Buttsworth DR, Jones TV (1998) A fast-response total temperature probe for unsteady compressible flows. J Eng Gas Turbines Power 120(4):694–702

5. Nagai H, Oumi S, Asai K, Nakaita K (2006) Effect of temperature sensitive paint layer on global heat transfer measurement in hypersonic flow. J Visual Soc Jpn 26(1):201–204

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