Investigation of effects of convergence and divergence half-angles on the performance of a nozzle for different operating conditions

Author:

Hamedi-Estakhrsar M. H.,Mahdavy-Moghaddam H.,Jahromi M.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Reference19 articles.

1. Quintao KK (2012) Design optimization of nozzle shapes for maximum uniformity of exit flow. M.S. Thesis, Florida International University

2. Mason ML, Putnam LE, Richard JR (1980) The effect of throat contouring on two dimensional converging-diverging nozzles at static condition. NASA technical paper 1704

3. Park KA, Choi YM, Choi HM, Cha TS, Yoon BH (2001) The evaluation of critical pressure ratios of sonic nozzles at low Reynolds numbers. Flow Meas Instrum 12:37–41

4. Paik JS, Park KA, Park JT (2000) Inter-laboratory comparison of sonic nozzles at KRISS. Flow Meas Instrum 11:339–344

5. Spotts N, Guzik S, Gaoz X (2007) A CFD analysis of compressible flow through convergent-conical nozzles. AIAA, New York

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