The aerodynamic forces on an oscillating two-dimensional wing in accelerated supersonic flight

dc.contributor.author	D. E. Davies	en_US
dc.date.accessioned	2014-10-21T15:55:48Z
dc.date.available	2014-10-21T15:55:48Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/R&M-3299	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3879
dc.description.abstract	The lift distribution on a two-dimensional wing oscillating in accelerated flight is obtained by solving the linearised partial differential equation for the velocity potential in the fluid flow about the wing and applying the linearised Bernoulli equation. Expressions for the total lift and moment are obtained as integrals in,)olving the upwash on the wing. Numerical values for the lift and moment on a heaving wing and on a pitching wing have been obtained when the forward acceleration of the wing is uniform.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The aerodynamic forces on an oscillating two-dimensional wing in accelerated supersonic flight	en_US