The Performance of Fan-shaped Hole Film Cooling on a Gas Turbine Blade at Transonic Conditon with High Freestream Turbulence
50th, Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 2012 ; Nashville, TN
Aerospace sciences meeting; including the new horizons forum and aerospace exposition 2012 ; 5342-5352
2012-01-01
11 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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