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

International Journal of Heat and Mass Transfer

Volumn 44, Issue 6, 2001, Pages 1223-1233

  Eckert, E R G ^a   Sakamoto, H ^a   Simon, T W ^a  

^a University of Minnesota   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYER; HEAT TRANSFER; MASS TRANSFER; TURBINE;

EID: 0035065517     PISSN: 00179310     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0017-9310(00)00175-7     Document Type: Article

References (21)

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2. Wärmeübergang, Diffusion und Verdunstung
3. Convective transport phenomena on the suction of a turbine blade including the influence of secondary flows near the endwall
4. STAN5: A program for numerical computation of two-dimensional internal and external boundary layer flows
5. Similarity analysis of model experiments for film cooling in gas turbines
6. On the dynamical theory of incompressible viscous fluids and the determination of the criterion
7. A review of mass transfer measurements using naphthalene sublimation
8. A new analogy function for the naphthalene sublimation technique to measure heat transfer coefficients on turbine airfoils
9. An experimental study to compare the naphthalene sublimation with the liquid crystal technique in compressible flow
10. Transient heat transfer experiments in a linear cascade via an insertion mechanism using the liquid crystal technique
11. Effectiveness of the gas turbine endwall fences in secondary flow control at elevated freestream turbulence levels
12. A new hue capturing technique for the quantitative interpretation of liquid crystal images used in convective heat transfer studies