In all numerical calculations for air take C₂ = 1.01 kJ/kg K and y = 1.4. (c) Using the relation To = T+ (u²+²)/(2Cp),
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In all numerical calculations for air take C₂ = 1.01 kJ/kg K and y = 1.4. (c) Using the relation To = T+ (u²+²)/(2Cp),
(c) Using the relation To = T+ (u²+²)/(2Cp), deduce the stagnation temperature equation in the form DTO pCp- = Dt Finally, write the D/Dt in component form for steady flow, assume constant viscosity, and simplify the viscous term in this equation by noting (by elementary rules of calculus) u Ju dy² = 2 Ә Oy (5) - (O)² ду