Oscillatory aerodynamic forces in linearised supersonic flow for arbitrary frequencies, planforms and mach numbers

dc.contributor.author	D. J. Allen	en_US
dc.contributor.author	D. S. Sadler	en_US
dc.date.accessioned	2014-10-21T15:56:23Z
dc.date.available	2014-10-21T15:56:23Z
dc.date.issued	1963	en_US
dc.identifier.other	ARC/R&M-3415	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/4000
dc.description.abstract	A method is described of performing a numerical integration to solve the integral equation connecting downwash an d velocity potential in linearised unsteady supersonic flow. Supersonic and subsonic leading edges and wakes are dealt with, and some practical results are given. By using this approach, a sufficiently general computer programme could deal accurately with kinked and curved edges.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Oscillatory aerodynamic forces in linearised supersonic flow for arbitrary frequencies, planforms and mach numbers	en_US