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Effect of NACA injection impeller and ducted head baffles on flight cooling performance of double-row radial engine in four-engine heavy bomber

机译：NaCa喷射叶轮和导管头挡板对四发动力重型轰炸机双排径向发动机飞行冷却性能的影响

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作者
Vensel, Joseph R;
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年度 1945
页码 1-14
总页数 14
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ENGINES-WRIGHT R-3350 (AMER ); COOLING TESTS; COOLING SYSTEMS-BOEING B-29; FLIGHT TESTS; IMPELLERS, FUEL-INJECTION-NACA; BAFFLES-ENGINE CYLINDERS;

机译：ENGINEs-WRIGHT R-3350（amER）;冷却测试;冷却系统 - 波音B-29;飞行测试; ImpELLERs，FUEL-INJECTION-NaCa; BaFFLEs-ENGINE CYLINDERs;

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6. Analysis of cooling limitations and effect of engine-cooling improvements on level-flight cruising performance of four-engine heavy bomber [O] . Marble Frank E., Miller Mahlon E., Bell E. Barton 1946

机译：分析冷却限制和发动机冷却改进对四发动机重型轰炸机水平飞行巡航性能的影响

Effect of NACA injection impeller and ducted head baffles on flight cooling performance of double-row radial engine in four-engine heavy bomber

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