A methodology for robust design of impingement cooled HSCT combustor liners
35th Aerospace Sciences Meeting and Exhibit ; 1997 ; Reno , NV , U.S.A.
1997-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
A Methodology for the Robust Cooling Design of an HSCT Combustor Liner
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