Numerical Conjugate Flow and Heat Transfer Investigation of a Transonic Convection-Cooled Turbine Guide Vane with Stress-Adapted Thicknesses of Different Thermal Barrier Coatings
38th, Aerospace sciences meeting ; 2000 ; Reno, NV
2000-01-01
ALL
Paper nos AIAA-2000-0001 to AIAA-2000-1076 with gaps
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 1999
|Conjugate Heat Transfer Analysis of a Cooled Turbine Vane Using the V2F Turbulence Model
Online Contents | 2007
|