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Experimental Investigation of Air-cooled Turbine Rotor Blade Temperatures in a Turbojet Engine Operating at Turbine-inlet Temperatures Up to 2580°R and Altitudes of 50,000 and 60,000 Feet

Henry O. Slone

出版	National Advisory Committee for Aeronautics, 1956
URL	http://books.google.com.hk/books?id=IlXyZwEACAAJ&hl=&source=gbs_api