Aerospace Engineering Lectures - Ballistic Entry and Heating, Aerospace Engineering Lecture 66

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stanton number entry heating atmospheric reentry aerodynamic heating in aircraft aerodynamic heating reynolds analogy in heat transfer Reynold's analogy heat shield space shuttle Heating in spacecraft space shuttle heat shield failure bluff body aerodynamics aerospace engineering course

Full Transcript

Heating rate and total heat generated during atmospheric entry of a spacecraft into the earth's atmosphere is explained. The Stanton number and Reynold's analogy is used to derive the expression for heat loss during atmospheric re-entry. The advantage of a blunt nose rather than a pointed nose is explained. #aerospaceengineering #spacecraft #aerospaceengineeringgatepreparation