NASA Technical Reports Server (NTRS) : A pdf

NASA Technical Reports Server (NTRS) : A

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Description of the Book:

The program input, coolant flow and heat transfer model, and the program output are discussed. As an example, sections of the suction and pressure sides of a high temperature, high pressure turbine vane are analyzed to show the effects of a thermal barrier coating. Compared to the uncoated design, the coating halves the required coolant flow, while simultaneously reducing metal outer temperatures by over 111 K

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 6/1/1978
• Year: 1978
• Book Topics/Themes: NASA Technical Reports Server (NTRS), COMPUTER PROGRAMS, FILM COOLING, THERMAL CONTROL COATINGS, TURBINE BLADES, COOLING SYSTEMS, ENGINE COOLANTS, HEAT TRANSFER, JET ENGINES

An excerpt captured from the PDF book