Numerical conjugate flow and heat transfer investigation of a transonic convection-cooled turbine guide vane with stress-adapted thicknesses of different thermal barrier coatings
New York, NY / American Inst. of Aeronautics and Astronautics [u.a.] (2000) [Contribution to a book, Contribution to a conference proceedings]
A collection of the 2000 ASME Wind Energy Symposium technical papers at the 38th AIAA Aerospace Sciences Meeting and Exhibit : Reno, NV, 10 - 13 January 2000
Page(s): 10 S.
- REPORT NUMBER: RWTH-CONV-179708