The heat/mass transfer analogy factor, Nu/Sh, for boundary layers on turbine blade profiles

Physics & Astronomy

• nu factor 100%
• turbine blades 84%
• mass transfer 62%
• boundary layers 59%
• Nusselt number 49%
• heat 45%
• profiles 37%
• heat transfer 35%
• Schmidt number 30%
• fluid mechanics 28%
• gas turbines 27%
• high Reynolds number 26%
• heat transfer coefficients 25%
• Prandtl number 24%
• coefficients 12%

Chemical Compounds

• Turbine 90%
• Nusselt Number 82%
• Heat Transfer 74%
• Mass Transfer 57%
• Heat 51%
• Prandtl Number 42%
• Schmidt Number 37%
• Sherwood Number 37%
• Fluid Mechanics 36%
• Reynolds Number 31%
• Transfer Coefficient 27%

Engineering & Materials Science

• Boundary layers 64%
• Mass transfer 61%
• Turbines 53%
• Nusselt number 46%
• Hot Temperature 33%
• Heat transfer 30%
• Fluid mechanics 27%
• Prandtl number 27%
• Heat transfer coefficients 21%
• Gas turbines 20%
• Reynolds number 19%