Evaluation of internal heat-transfer coefficients for impingement-cooled turbine airfoils.
Author:
Affiliation:
1. Allison Division of General Motors Corporation, Indianapolis, Ind.
2. Purdue University, Lafayette, Ind.
3. Midwest Applied Science Corporation, West Lafayette, Ind.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference7 articles.
1. Investigations of Heat-Transfer Coefficients for Air Flow Through Round Jets Impinging Normal to a Heat-Transfer Surface
2. Heat Transfer Characteristics of Impinging Two-Dimensional Air Jets
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