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Preliminary transonic performance results for solid and slotted turbojet nacelle afterbodies incorporating fixed divergent jet nozzles designed for supersonic operation

机译：固体和开槽涡轮喷气发动机舱后体的初步跨音速性能结果，其中包含设计用于超音速操作的固定发散喷嘴

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Transonic performance of three turbojet nozzle- afterbody configurations

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作者
Runckel, J. F.;
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年度 1958
页码 1-44
总页数 44
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CONFIGURATIONS; AFTERBODIES; AFTERBURNING; DIVERGENT NOZZLES; JET NOZZLES; NACELLES; TURBOJET ENGINES; AFTERBODY; JET NOZZLE; TURBOJET ENGINE;

机译：空气动力学配置; aFTERBODIEs;加力;分散喷嘴; JET NOZZLEs;发动机舱;涡轮发动机;床尾; JET NOZZLE;涡轮发动机;

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专利

1. A Computational Analysis of Unsteady Transonic/Supersonic Flows Over Backward Facing Step in Air Jet Nozzle [J] . Sang Dug Kim, Jeong Ill Seo, Dong Joo Song Journal of Mechanical Science and Technology . 2007,第2期

机译：喷气喷嘴后向台阶上非定常跨音速/超音速流的计算分析
2. A computational analysis of unsteady transonic/supersonic flows over backward facing step in air jet nozzle [J] . Sang Dug Kim, Jeong Ill Seo, Dong Joo Song Journal of Mechanical Science and Technology . 2007,第2期

机译：射流喷嘴后向台阶上非定常跨音速/超音速流的计算分析
3. A Numerical analysis of Transonic/supersonic Flows in the Axisymmetric Main Nozzle of an Air-Jet Loom [J] . T.H.Oh, S.D.Kim, D.J.Song Textile Research Journal . 2001,第9期

机译：喷气织机轴对称主喷嘴中跨音速/超音速流的数值分析
4. JET NOISE REDUCTION BY A CROSS WIRE DEVICE IN SUPERSONIC JET ISSUING FROM A CONVERGENT-DIVERGENT NOZZLE [C] . Y. H. Kweon, Y. Miyazato, T. Aoki, International Symposium on Flow Visualization . 2004

机译：通过收敛沟槽发布超音速喷射器中的交叉线装置的射流减少
5. Plume and performance measurements on a plug nozzle for supersonic business jet applications. [D] . Sandroni, Alexander Michael. 2009

机译：用于超音速公务机应用的旋塞喷嘴上的羽流和性能测量。
6. An experimental study of flow in a nozzle designed to provide a parallel jet at supersonic speed [O] . Hennessey Thomas Vincent, Duke John Morgan Jr., Duke John Morgan 1946

机译：在喷嘴中以超音速提供平行射流的流动的实验研究

Preliminary transonic performance results for solid and slotted turbojet nacelle afterbodies incorporating fixed divergent jet nozzles designed for supersonic operation

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