CERES > School of Engineering (SoE) (2001-July 2014) > College of Aeronautics Reports >

Please use this identifier to cite or link to this item: http://dspace.lib.cranfield.ac.uk/handle/1826/7127

Document Type: Report
Title: Application of the linear perturbation theory to compressible flow about bodies of revolution
Authors: Young, A. D.
Kirkby, S.
Issue Date: Sep-1947
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…
URI: http://dspace.lib.cranfield.ac.uk/handle/1826/7127
Appears in Collections:College of Aeronautics Reports

Files in This Item:

File Description SizeFormat
COA_Report_No_11_SEP_1947.pdf2.71 MBAdobe PDFView/Open

SFX Query

Items in CERES are protected by copyright, with all rights reserved, unless otherwise indicated.