Works matching DE "TURBOJET plane engine compressors"

A method for calculating inlet distortion effects on stability of split-flow fans.

Published in:

Aeronautical Journal, 2009, v. 113, n. 1147, p. 591, doi. 10.1017/S0001924000003250

By:

• Khaleghi, H.;
• Doulgeris, G.;
• Boroomand, M.;
• Pilidis, P.;
• Tousi, A. M.

Publication type:

Article