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Implementation and further application of refined transition prediction methods for turbomachinery and other aerodynamic flows

AM Savill and Erik Dick (UGent)
(2001) ERCOFTAC BULLETIN. p.58-60
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Please use this url to cite or link to this publication:

MLA
Savill, AM, and Erik Dick. “Implementation and Further Application of Refined Transition Prediction Methods for Turbomachinery and Other Aerodynamic Flows.” ERCOFTAC BULLETIN, edited by DR Emerson, no. 50, European Research Community on Flow, Turbulence and Combustion (ERCOFTAC), 2001, pp. 58–60.
APA
Savill, A., & Dick, E. (2001). Implementation and further application of refined transition prediction methods for turbomachinery and other aerodynamic flows. ERCOFTAC BULLETIN, (50), 58–60.
Chicago author-date
Savill, AM, and Erik Dick. 2001. “Implementation and Further Application of Refined Transition Prediction Methods for Turbomachinery and Other Aerodynamic Flows.” Edited by DR Emerson. ERCOFTAC BULLETIN, no. 50: 58–60.
Chicago author-date (all authors)
Savill, AM, and Erik Dick. 2001. “Implementation and Further Application of Refined Transition Prediction Methods for Turbomachinery and Other Aerodynamic Flows.” Ed by. DR Emerson. ERCOFTAC BULLETIN (50): 58–60.
Vancouver
1.
Savill A, Dick E. Implementation and further application of refined transition prediction methods for turbomachinery and other aerodynamic flows. Emerson D, editor. ERCOFTAC BULLETIN. 2001;(50):58–60.
IEEE
[1]
A. Savill and E. Dick, “Implementation and further application of refined transition prediction methods for turbomachinery and other aerodynamic flows,” ERCOFTAC BULLETIN, no. 50, pp. 58–60, 2001.
@article{143418,
  author       = {{Savill, AM and Dick, Erik}},
  editor       = {{Emerson, DR}},
  journal      = {{ERCOFTAC BULLETIN}},
  language     = {{eng}},
  number       = {{50}},
  pages        = {{58--60}},
  publisher    = {{European Research Community on Flow, Turbulence and Combustion (ERCOFTAC)}},
  title        = {{Implementation and further application of refined transition prediction methods for turbomachinery and other aerodynamic flows}},
  year         = {{2001}},
}