Application of the linear perturbation theory to compressible flow about bodies of revolution

dc.contributor.authorYoung, A. D.
dc.contributor.authorKirkby, S.
dc.date.accessioned2012-05-08T18:35:59Z
dc.date.available2012-05-08T18:35:59Z
dc.date.issued1947-09
dc.description.abstractThe linearised theory is developed in some detail in order to clarify the differences between two-dimensional and axi-symmetric flow. In agreement with other authors it is concluded that the perturbation velocity on a thin body of revolution in compressible flow is 1/β2 times the perturbation velocity in incompressible flow on a thinner body at reduced incidence obtained by reducing the lateral dimensions of the original body in the ratio (3:1). This result is applied to a representative family of streamline bodies of revolution at zero incidence. Continues…en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7127
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries11en_UK
dc.titleApplication of the linear perturbation theory to compressible flow about bodies of revolutionen_UK
dc.typeReporten_UK

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