1995
DOI: 10.1007/bf02079401
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Designing three-dimensional nozzles to achieve near-uniform supersonic or hypersonic flow in the rectangular exit section

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Cited by 1 publication
(14 citation statements)
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“…Generally the execution time for design problems is quite high despite the power of calculator used since there is repetition of calculation. The methods developed for determining the contours of the three dimensional nozzles are based on the determination of the internal stream lines using the definition of the stream function [1][2][3][4][5][6]. As the flow is considered as perfect and nonviscous, the stream lines can represent rigid surfaces and hence a wall shape of obstacles [7].…”
Section: Introductionmentioning
confidence: 99%
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“…Generally the execution time for design problems is quite high despite the power of calculator used since there is repetition of calculation. The methods developed for determining the contours of the three dimensional nozzles are based on the determination of the internal stream lines using the definition of the stream function [1][2][3][4][5][6]. As the flow is considered as perfect and nonviscous, the stream lines can represent rigid surfaces and hence a wall shape of obstacles [7].…”
Section: Introductionmentioning
confidence: 99%
“…As the flow is considered as perfect and nonviscous, the stream lines can represent rigid surfaces and hence a wall shape of obstacles [7]. In our case these stream lines can represent the wall of the nozzle [1][2][3][4][5][6]. The use of these methods requires a very high computational time since the search of the points of the stream lines is based on the use of the segments in upward and downward characteristics from the developed internal mesh in the axisymmetric nozzle, which becomes impossible for fine meshes, in a time when a fine mesh give a high precision.…”
Section: Introductionmentioning
confidence: 99%
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