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Titlebook: Shock Waves @ Marseille I; Hypersonics, Shock T Raymond Brun,Lucien Z. Dumitrescu Conference proceedings 1995 Springer-Verlag Berlin Heidel

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書目名稱Shock Waves @ Marseille I
副標(biāo)題Hypersonics, Shock T
編輯Raymond Brun,Lucien Z. Dumitrescu
視頻videohttp://file.papertrans.cn/867/866675/866675.mp4
圖書封面Titlebook: Shock Waves @ Marseille I; Hypersonics, Shock T Raymond Brun,Lucien Z. Dumitrescu Conference proceedings 1995 Springer-Verlag Berlin Heidel
描述Recently, there have been significant advances in the fields of high-enthalpy hypersonic flows, high-temperature gas physics, and chemistry shock propagation in various media, industrial and medical applications of shock waves, and shock-tube technology. This series contains all the papers and lectures of the 19th International Symposium on Shock Waves held in Marseille in 1993. They are published in four topical volumes, each containing papers on related topics, and preceded by an overview written by a leading international expert. The volumes may be purchased independently.
出版日期Conference proceedings 1995
關(guān)鍵詞Oscillation; combustion; enthalpy; entropy; high-pressure; imaging techniques; numerical analysis; numerica
版次1
doihttps://doi.org/10.1007/978-3-642-78829-1
isbn_softcover978-3-642-78831-4
isbn_ebook978-3-642-78829-1
copyrightSpringer-Verlag Berlin Heidelberg 1995
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Interference and Transient Effects on Compression Ramp Flows at Hypersonic Mach Numbersflow adjustment have been examined, and the development of criteria to predict separated flow establishment times discussed. During the initial experiments, nozzle exit compression waves were found to be a corrupting influence. Methods of detecting this interference, and its effects, have been assessed.
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Effects of Leading-Edge Bluntness on Control Flap Effectiveness at Hypersonic Speedsin a hypersonic gun tunnel facility at .. = 8.2 and ../. = 9.0 × 10.. The flow structure over a low aspect ratio flat plate with a full span trailing edge flap has been investigated using high speed Schlieren photography as well as surface pressure and heat transfer measurements.
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The Boundary Layer on a Sharp Cone in High-Enthalpy Flowaminar layer, heat flux levels are higher in air than in nitrogen because of a larger heat release from oxygen recombination at the wall. By varying the specific reservoir enthalpy in air and N., and from measurements in CO., it is found that real-gas effects stabilize the boundary layer.
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978-3-642-78831-4Springer-Verlag Berlin Heidelberg 1995
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Shock Tube Investigations of Combustion Phenomena in Supersonic FlowsA survey is given of recent combustion dynamics research using shock tubes. There are three different fields where phenomena in supersonic gas flows resulting from chemical heat release are of particular interest:
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A Life with Shock Waves (Ernst Mach Memorial Lecture)iscovered, which delays BL separation. Shock focusing, amplification, and stability were investigated; a “shock nozzle” was devised, and also an improved version of the spiral contraction. Recently, the author joined Prof. Raymond Brun’s Marseille team working on the development of a new Stalker-tub
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