Pressure loss tests on a flat-bladed turbine nozzle cascade

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DOI	Resolve DOI: https://doi.org/10.4224/40003998
Author	Search for: Bassett, R.W.¹
Affiliation	National Research Council Canada. Division of Mechanical Engineering
Format	Text, Memorandum
Physical description	23 p.
Abstract	This Memorandum presents the results of pressure loss tests made to date on a cold-air, low-pressure, rig simulating a segment of a tip turbine stator assembly and supply duct, and characterized by flat-plate nozzle blades. A range of pitch/chord ratios has been tested, and the effects on performance of the nozzle shape and blade trailing edge thickness have been briefly investigated.
Date published	1960-07-07
Publisher	National Research Council of Canada
Series	Laboratory Memorandum (National Research Council of Canada. Division of Mechanical Engineering. Engine Laboratory), no. NRC-ENG-25 (7 July 1960).
Language	English
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Record identifier	aef72cb0-5f61-4562-b116-145b043aeb10
Record created	2026-04-08
Record modified	2026-04-08

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