@article{wanchai_asvapoositkul_three-dimensional_nodate,
	title = {Three-{Dimensional} {Turbomachinery} {Inverse} {Blade} {Design}: {An} {Application} to {Axial} {Flow} {Compressor}},
	abstract = {The computational method based on three-dimensional inverse design in inviscid flow is applied to the design of 0.78 m diameter single stage axial flow compressor. By applying this method, the blade shape is computed for a specified distribution of swirl distribution. A useful design of the method is that the blade shape is compatible with prescribe the surface velocity. Therefore, an improvement in the performance is expected. The experimental data showed that the design blade gave excellent agreements from those of the computed results. The flow in the designed compressor rotor closely approximates that of viscous analysis code and shows no breakdown of the flow within the designed blade profile.},
	language = {en},
	author = {{Wanchai Asvapoositkul} and Amphonkiat, Thanongsak},
	pages = {5},
}

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