Article contents
On the theory of a cascade of stalled aerofoils
Published online by Cambridge University Press: 09 April 2009
Summary
A mathematical theory of the separating flow past a cascade of aerofoils is developed. The flow is assumed to be inviscid, incompressible and twodimensional. The wakes are represented by regions of stationary fluid, which could, in the general case, maintain a pressure gradient, although much of the theory is developed for the case of constant wake pressure.
- Type
- Research Article
- Information
- Copyright
- Copyright © Australian Mathematical Society 1960
References
- 2
- Cited by