This paper presents the results of a numerical simulation of the time-averaged inviscid flow field through the blade rows of a multiblade row turboprop configuration. The governing equations are outlined along with a discussion of the solution procedure and coding strategy. Numerical results obtained from a simulation of the flow field through a modern high-speed turboprop will be shown.
A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller
- Views Icon Views
- Share Icon Share
- Search Site
Celestina, M. L., Mulac, R. A., and Adamczyk, J. J. (October 1, 1986). "A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller." ASME. J. Turbomach. October 1986; 108(2): 187–193. https://doi.org/10.1115/1.3262036
Download citation file: