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Cooling Techniques for Hypersonic Vehicles by MD. JAMINUR RAHMAN KHALID 2003110 is a document available to read on EtoBox.

What is Cooling Techniques for Hypersonic Vehicles about?

This paper investigates the feasibility of cooling hypersonic vehicle leading-edge structures using liquid metal heat pipes and surface mass transfer techniques. A transient, finite difference-based cooling model was developed and demonstrated on a hypothetical aerospace plane wing leading-edge section, showing that these cooling methods effectively limit maximum surface temperatures and structural temperature gradients. The study concludes that combining these techniques is a viable approach for managing s

Author

MD. JAMINUR RAHMAN KHALID 2003110

Language

EN