NASA NTRS · 19890041035
Unsteady Euler cascade analysis
Abstract
The results of an investigation of the rotor-stator interaction phenomena in turbomachines are presented. Numerical study was carried out by solving the unsteady Euler equations in the blade-to-blade direction for a variety of cascade geometries. The problem of uneven rotor and stator blades is addressed by adopting the tilted time domain technique. Computed solutions are presented and discussed for a NACA 0012 type cascade and the first stage fuel turbopump of the Space Shuttle Main Engine (SSME).
Keep this discovery
Explore connections, maps & timelines
Liu, Jong-Shang, Sockol, Peter M.. 1989-01-01. Unsteady Euler cascade analysis. https://ntrs.nasa.gov/citations/19890041035
Cite the original work for its findings. Save a collection to share your selection of sources.