An engineering method for modeling the interaction of circular bodies and very low aspect ratio cruciform wings at supersonic speeds
An engineering method using a 2D unsteady potential formulation (called the free vortex model or FVM) has been developed to predict the normal force, centre-of-pressure and vortex position for cruciform wing-body combinations in the “plus” orientation, at supersonic speeds and cross flow Mach numbers...
| Main Author: | |
|---|---|
| Published: |
University of the West of England, Bristol
2013
|
| Subjects: | |
| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.589106 |