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Effectiveness of a Turbojet Tubular Combustor in Screening the Turbine from Foreign Objects (1955)
NASA Technical Reports Server (NTRS) · leaf 11
11 NACA EM E55E16 -Slots, approx. ^ f 3 . Air-intake holes, diam, in. ^ ^ * C-35309 Figure 1. - Inner liner for J47 comhustion chamber. … Figure 2. - Simulated combustor assembly used in tests.NASA Technical Reports Server (NTRS)
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