Assessment of binary PSP technique for film cooling effectiveness measurement on nozzle vane cascade with cutback trailing edge

Author:

Barigozzi GiovannaORCID,Mucignat Claudio,Abdeh Hamed,Scandella Davide,Dolci Giorgio

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Aerospace Engineering,Nuclear Energy and Engineering,General Chemical Engineering

Reference31 articles.

1. Gas Turbine Heat Transfer and Cooling Technology;Han,2000

2. S. Friedrichs, H.P. Hodson, The ammonia and diazo surface coating technique for measuring adiabatic film cooling effectiveness, in: 12th Symposium on Measuring Techniques for Transonic and Supersonic Flow in Cascades and Turbomachines, 12-13 September 1994, Prague, The Czech Republic, 1994.

3. L. Zhang, M. Baltz, R. Pudupatty, M. Fox, Turbine nozzle film cooling study using the Pressure Sensitive Paint (PSP) Technique, ASME paper 99-GT-196, 1999, http://doi.org/10.1115/99-GT-196.

4. Surface pressure measurements using luminescent coatings;Bell;Ann. Rev. Fluid Mech.,2001

5. Turbine blade film cooling using PSP technique;Han;Front. Heat Mass Transfer.,2010

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