Affiliation:
1. Massachusetts Institute of Technology, Cambridge, MA
Abstract
A previously described inviscid design technique has been substantially improved to allow the generation of either shock free, weak shock or low total pressure loss supersonic rotor cascade designs. Improvements have been introduced in inflow-outflow boundary conditions, imposition of geometric constraints and in shock pressure rise specifications. Calculation examples are presented for pre-compression type rotor designs.
Publisher
American Society of Mechanical Engineers
Cited by
4 articles.
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