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Inlet Flow Field Investigation. Part 1: Transonic Flow Field Survey

机译：进水流场调查。第1部分：跨音速流场测量

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A wind tunnel investigation was conducted to determine the local inlet flow field characteristics of an advanced tactical supersonic cruise airplane. A data base for the development and validation of analytical codes directed at the analysis of inlet flow fields for advanced supersonic airplanes was established. Testing was conducted at the NASA-Langley 16-foot Transonic Tunnel at freestream Mach numbers of 0.6 to 1.20 and angles of attack from 0.0 to 10.0 degrees. Inlet flow field surveys were made at locations representative of wing (upper and lower surface) and forebody mounted inlet concepts. Results are presented in the form of local inlet flow field angle of attack, sideflow angle, and Mach number contours. Wing surface pressure distributions supplement the flow field data.

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作者
Yetter, J. A.; Salemann, V.; Sussman, M. B.;
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年度 1984
页码 p.1-122
总页数 122
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Flow distribution; Inlet flow; Supersonic cruise aircraft research; Transonic flow; Angle of attack; Backwash; Data bases; Flow characteristics; Mach number; Pressure distribution; Wind tunnel tests; Wings;

机译：流量分配;进气流量;超音速巡航飞机研究;跨音速流量;迎角;反冲洗;数据库;流量特性;马赫数;压力分布;风洞试验;翅膀;

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专利

1. Aerothermal Study of the Unsteady Flow Field in a Transonic Gas Turbine With Inlet Temperature Distortions [J] . S. Salvadori, F. Montomoli, F. Martelli, Journal of turbomachinery . 2011,第3期

机译：进气温度畸变的跨音速燃气轮机非定常流场的气热研究
2. Independent Two-Fields Solution for Full-Potential Unsteady Transonic Flows [J] . A. Parrinello and P. Mantegazza AIAA Journal . 2010,第7期

机译：全势非定常跨音速流的独立两场解决方案
3. Independent Two-Fields Solution for Full-Potential Unsteady Transonic Flows [J] . A. Parrinello, P. Mantegazza AIAA Journal . 2010,第7期

机译：全势非定常跨音速流的独立两场解决方案
4. TRANSONIC AXIAL COMPRESSORS WITH TOTAL PRESSURE INLET FLOW FIELD DISTORTIONS [C] . Andreas Lesser, Reinhard Niehuis ASME turbo expo: turbine technical conference and exposition . 2014

机译：具有总压力入口流场畸变的超音速轴向压缩机
5. Experimental investigation of the flow field in a transonic, axial flow compressor with respect to the development of blockage and loss [D] . Suder, Kenneth Lee 1996

机译：跨音速轴流式压缩机流场关于阻塞和损失发展的实验研究
6. Rapid protein separation and diffusion coefficient measurement by frit inlet flow field-flow fractionation. [O] . M. K. Liu, P. Li, J. C. Giddings 1993

机译：通过熔块入口流场流分馏快速蛋白质分离和扩散系数测量。
7. Flow field surveys in a transonic compressor prior to inlet steam ingestion tests [O] . Villescas Ivan J. 2005

机译：进汽蒸汽摄入测试之前，在跨音速压缩机中进行流场调查

Inlet Flow Field Investigation. Part 1: Transonic Flow Field Survey

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