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Pressure measurements on a sharply converging fuselage afterbody with jet on and off at Mach numbers from 0.8 to 1.6

机译：在急剧收敛的机身后面进行压力测量，喷射打开和关闭，马赫数为0.8到1.6

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Stoney, William E , Jr; Katz, Ellis;
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年度 1950
页码 1-20
总页数 20
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Streak Line Pattern of Supersonic Transverse Jet into Mach 6 Freestream over a Sharp Cone [J] . Dhananjaya Rao G., Swaminathan S., Rathakrishnan E. Journal of visualization . 2008,第4期

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3. ENTHALPY INCREMENT MEASUREMENTS ON LIQUID ETHANE BETWEEN THE TEMPERATURES 146.0 K AND 256.2 K, AT PRESSURES (APPROXIMATE-TO-1.6, 3.20, AND 5.07) MPA [J] . Grini PG., Brendeng E., Owren GA., The Journal of Chemical Thermodynamics . 1996,第6期

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4. Pressure-sensitive paint measurements of the pressure field about a sonic jet injected transversely into a mach 1.6 freestream [C] . D.E.Everett, J.C.Dutton, M.J.Morris AIAA 33rd Aerospace Seicnces Meeting and Exhibit January 9-12, 1995/Reno, NV . -1

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5. Hot-wire measurements of instability waves on sharp and blunt cones at Mach 6. [D] . Rufer, Shann J. 2005

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6. Hydrostatic Pressure and Temperature Measurements Using an In-Line Mach-Zehnder Interferometer Based on a Two-Mode Highly Birefringent Microstructured Fiber [O] . Gabriela Statkiewicz-Barabach, Jacek Olszewski, Pawel Mergo, 2017

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7. Pressure measurements in the heat shield region of 1/80 scale PSLV model In the mach number range of 0.8 to 4.0udud [O] . Sajeer Ahmed, Selvarajan S 1985

机译：1/80比例PSLV模型的隔热屏区域中的压力测量，马赫数范围为0.8至4.0 ud ud

Pressure measurements on a sharply converging fuselage afterbody with jet on and off at Mach numbers from 0.8 to 1.6

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