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COMPARATIVE STUDY OF THE HEAT TRANSFER OF A NOZZLE BLADE PROFILE IN A WIND TUNNEL AND IN AN AIR TURBINE

DYBAN, Y. P., KUROSH, V. D · 1974 · 1 picture

A 1974 NASA-distributed technical report by Y. P. Dyban and V. D. Kurosh comparing heat transfer measurements on a turbine nozzle blade profile in a wind tunnel and in an air turbine, written for propulsion and heat-transfer engineers. The single illustration is a coarse line drawing of a curved blade section with numbered leader lines marking instrument leads and hatched surfaces, useful as a schematic diagram with callout numbering.

Flight safety · Payloads · Space shuttles · Spacecraft design · Spacecrews · Cost reduction · Project management · Systems engineering

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