Turbine inlet protection system concept design using CFD technology
30th Joint Propulsion Conference and Exhibit ; 1994 ; Indianapolis , IN , U.S.A.
1994-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Inlet protection for aircraft gas turbine engines
Engineering Index Backfile | 1954
|INLET PROTECTION FOR AIRCRAFT GAS TURBINE ENGINES
SAE Technical Papers | 1954
|Inlet/TBCC/Nozzle Integration Concept Design
AIAA | 2008
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