NASA NTRS · 19930093861
Flat Plate Cascades at Supersonic Speed
Abstract
A brief review of exact two-dimensional supersonic flow theory and Ackeret's linearized theory are first presented. The lift and drag coefficients of a cascade of flat plates are calculated exactly and compared to those obtained using the linearized theory. The forces on the cascade are determined for unsteady inlet flow. The flat plate cascade theory is extended to compute the efficiency of a supersonic propeller with friction and finite blade thickness.
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
El Badrawy, Rashad M. 1956-05-01. Flat Plate Cascades at Supersonic Speed. https://ntrs.nasa.gov/citations/19930093861
Cite the original work for its findings. Save a collection to share your selection of sources.