Project Description

The spike mode of stall in transonic compressors, and the control of stall point location using tip injection flow control remain areas of research. The study considered here will endeavor to reveal details of the interaction of aerodynamic phenomena that enable tip injection to delay stall, that are not presently well understood.

Allocation History

Source Hours Start Date End Date
DD2,5002014-07-012015-07-31
DD2,000,0002014-01-012015-07-31
DD1,000,0002013-10-042013-12-31