Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line (Q431755)
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scientific article; zbMATH DE number 6051604
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line |
scientific article; zbMATH DE number 6051604 |
Statements
Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line (English)
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2 July 2012
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equalizing nozzle contour
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intersections of \(C^{+}\) or \(C^{
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}\)-characteristics
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Mach number at the nozzle exit
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the most rapid flow acceleration in the case of a curvilinear sonic line
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