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About this Engineering article
Numerical Predictions of Stanton Numbers, Skin Friction Coefficients, Aerodynamic Losses, and Reynolds Analogy Behavior for a Transsonic Turbine Vane by Zhang, Q.; Ligrani, P. M. is a Engineering article available to read on EtoBox.
It is typically read by researchers, students, and practitioners in Engineering.
- Author
- Zhang, Q.; Ligrani, P. M.
- Publisher
- Taylor and Francis Group; Informa UK (Taylor & Francis); Taylor & Francis; Informa UK Limited (ISSN 1040-7782)
- Published
- 2006
- Field
- Engineering (Physical Sciences)