NUMERICAL AND EXPERIMENTAL STUDY OF FILM COOLING EFFECTIVENESS AND TOTAL PRESSURE LOSS FOR A REALISTIC CASCADE WITH AN ANNULAR ENDWALL
49th, Aerospace sciences meeting; 49th AIAA Aerospace Sciences meeting including the New Horizons Forum and Aerospace Exposition 2011 ; 2011 ; Orlando, FL
2011-01-01
14 pages
Includes bibliographical references and index
Aufsatz (Konferenz)
Englisch
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Aerodynamic Implications of Endwall and Profile Film Cooling in a Transonic Annular Cascade
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