Aerospace
Technical Paper

Flow Simulations for an Aft-Mounted Propfan Using Euler Equations

861718

10/1/1986

Event
SAE Aerospace Technology Conference and Exposition
Authors
N. J. Yu The Boeing Company, Seattle, Washington
K. Kusunose The Boeing Company, Seattle, Washington
H. C. Chen The Boeing Company, Seattle, Washington
D. M. Sommerfield The Boeing Company, Seattle, Washington
Abstract
Content
A new transonic flow analysis program based on the solution of Euler equations has been developed. The program is capable of analyzing the flow over a complete wing/body/tail/aft-mounted propfan configuration at arbitrary freestream conditions. Computed results for an advanced aft-mounted propfan configuration with and without propeller are reported in this paper.
Meta Tags
Topics
Wings
Propellers and rotors
Affiliated or Co-Author
The Boeing Company, Seattle, Washington
Details
DOI
https://doi.org/10.4271/861718
Citation
Yu, N., Kusunose, K., Chen, H., and Sommerfield, D., "Flow Simulations for an Aft-Mounted Propfan Using Euler Equations," SAE Aerospace Technology Conference and Exposition, Long Beach, California, United States, October 13, 1986, https://doi.org/10.4271/861718.
Additional Details
Publisher
SAE International
Published
10/1/1986
Product Code
861718
Content Type
Technical Paper
Language
English