Application of the linear perturbation theory to compressible flow about bodies of revolution
dc.contributor.author | Young, A. D. | |
dc.contributor.author | Kirkby, S. | |
dc.date.accessioned | 2012-05-08T18:35:59Z | |
dc.date.available | 2012-05-08T18:35:59Z | |
dc.date.issued | 1947-09 | |
dc.description.abstract | The 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.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7127 | |
dc.language.iso | en | en_UK |
dc.publisher | College of Aeronautics, Cranfield | en_UK |
dc.relation.ispartofseries | College Report | en_UK |
dc.relation.ispartofseries | 11 | en_UK |
dc.title | Application of the linear perturbation theory to compressible flow about bodies of revolution | en_UK |
dc.type | Report | en_UK |