scientific article; zbMATH DE number 3111679
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Publication:5850276
zbMath0065.41303MaRDI QIDQ5850276
Publication date: 1955
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Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line ⋮ Thrust nozzle optimization including boundary layer effects ⋮ Analysis of the thrust characteristics of jet nozzles designed by various methods ⋮ Construction of compact nonsymmetric nozzles of maximal thrust for given lift ⋮ Variational problems for supersonic bodies of revolution and nozzles
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