Asymptotic Separation from Slender Cones at Incidence
- 1 January 1987
- book chapter
- Published by Springer Nature
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Steady and Unsteady Boundary-Layer SeparationAnnual Review of Fluid Mechanics, 1986
- Asymmetric Vortex Formation from Cones at Incidence – a Simple Inviscid ModelAeronautical Quarterly, 1982
- Improved calculations of leading-edge separation from slender, thin, delta wingsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1968
- A theory of the flow past a slender delta wing with leading edge separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1959