Studies in hypersonic viscous interactions

dc.contributor.advisor	Clarke, J. F.
dc.contributor.author	Murthy, A. V.
dc.date.accessioned	2023-05-04T12:34:08Z
dc.date.available	2023-05-04T12:34:08Z
dc.date.issued	1972-12
dc.description.abstract	The literature on the leading edge viscous interaction phenomena has "been reviewed. Theoretical studies of the leading edge bluntness and the boundary - layer displace¬ment effects have been made by using a combination of tangent wedge + centrifugal force pressure law relation and also using the 2nd order tangent wedge formula suggested by Lees . These analyses, when applied to concave surfaces show a mild oscillatory behaviour compared to the highly oscillatory results of Cheng's theory. Further, an integral approach due to Chernyi has been applied to concave surface flows and the damping of the oscillations present in Cheng’s theory is demonstrated. Experiments have been conducted at a Mach number Of 1 2 .2 in a gun tunnel, on flatplates and on a concave surface with a sharp leading edge. The results are compared with the predictions of various interaction theories.	en_UK
dc.description.coursename	PhD	en_UK
dc.identifier.uri	https://dspace.lib.cranfield.ac.uk/handle/1826/19591
dc.language.iso	en	en_UK
dc.title	Studies in hypersonic viscous interactions	en_UK
dc.type	Thesis	en_UK

Files

Now showing 1 - 1 of 1

Now showing 1 - 1 of 1