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Altitude-wind-tunnel investigation of tail-pipe burner with converging conical burner section on J35-A-5 turbojet engine

机译：J35-a-5涡轮喷气发动机锥形燃烧器截面尾管燃烧器的高空 - 风洞调查

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An investigation of turbojet-engine thrust augmentation by means of tail-pipe burning has been conducted in the NACA Lewis altitude wind tunnel.

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作者
Thorman, H Carl; Campbell, Carl E;
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年度 1950
页码 1-65
总页数 65
原文格式 PDF
正文语种 eng
中图分类工业技术;
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Altitude-wind-tunnel investigation of tail-pipe burner with converging conical burner section on J35-A-5 turbojet engine

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