1967
DOI: 10.1007/bf01027359
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Supersonic flow past a gas jet obstacle emerging from a plate

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1971
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Cited by 44 publications
(7 citation statements)
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“…A number of investigations aimed at the development of thrust vector control systems were carried out in the 1960s to study the pressure distribution in the region around the injector and the resulting normal force and pitching moment. 4,11,12 Several researchers 10,11,[13][14][15][16][17][18] analyzed this flow field through analytical models and experiments. However, these efforts have been only partially successful due in large part to the difficulty of experimentally measuring the local flow without disrupting it and in part, due to the inherent complexity of the flow physics involved.…”
Section: Introductionmentioning
confidence: 99%
“…A number of investigations aimed at the development of thrust vector control systems were carried out in the 1960s to study the pressure distribution in the region around the injector and the resulting normal force and pitching moment. 4,11,12 Several researchers 10,11,[13][14][15][16][17][18] analyzed this flow field through analytical models and experiments. However, these efforts have been only partially successful due in large part to the difficulty of experimentally measuring the local flow without disrupting it and in part, due to the inherent complexity of the flow physics involved.…”
Section: Introductionmentioning
confidence: 99%
“…There are similarities between the injection jet and a solid obstacle. In [3,4,5] it was used analytical methods for considered the issue. In fact, the pattern formed in the case of the injection jet is similar to the flow pattern in the case of installation of the flow path blunt axially symmetric rigid body.…”
Section: Resultsmentioning
confidence: 99%
“…The dimensions of the zones of p e r t u r b e d flow in the nozzles during the experiments were determined by three methods; from the distribution of the static pressure in the transverse sections of the nozzle; from the tracks of the flow in the visual representation compound on the wall of the nozzle in the perturbed flow zone [4];…”
Section: The Methods Of the Experimentsmentioning
confidence: 99%