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Experimental and analytical sonic nozzle discharge coefficients for Reynolds numbers up to 8,000,000 (1974)

Szaniszlo, A. J.

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Publication Date: 2019-07-13

Description: Sonic discharge coefficients are presented for two different geometry flow nozzles using nitrogen gas at high pressures where real-gas corrections are significant. Throat Reynolds number range extended up to 8,000,000. Experimentally obtained coefficients for a nozzle with a continuous and finite radius of curvature agreed with those obtained analytically to within 0.2 per cent. Experimental coefficients for a long-radius ASME nozzle agreed to within 0.25 per cent to an empirical equation representing the most probable subsonic discharge coefficient.

Keywords: AERODYNAMICS

Type: ASME PAPER 74-WA/FM-8 , American Society of Mechanical Engineers, Winter Annual Meeting; Nov 17, 1974 - Nov 22, 1974; New York, NY

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