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Validation of axial compressor results

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May 6, 2021, 04:36	Validation of axial compressor results	#1
pb123 New Member Pramod Join Date: May 2021 Posts: 1 Rep Power: 0	I intended to use axial compressor blade geometry, NACA 65-1210, however, in journal articles I haven't got compressor map for this blade geometry for the validation purpose. I got the compressor map for NACA 65-306. I have modelled NACA 65-306 blade geometry and validated the same. Now, can I use NACA 65-1210 blade to work on my problem? Or do I have to use NACA 65-306? Kindly provide your opinion.

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blade & aerofoil, blade geometry, validation

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