Numerical and Experimental Investigations of Boundary Layer Separation Control by Means of Synthetic Jets in Low Pressure Turbine Adverse Pressure Gradient Conditions
International Symposium; 20th, Air breathing engines; ISABE 2011 ; 2011 ; Gothenburg, Sweden
01.01.2011
10 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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