Supersonic blading

Details Supersonic blading Supersonic blading

F - Mech Eng,Light,Heat,Weapons

02

K

170/81

F02K 3/00 (2006.01) F04D 21/00 (2006.01)

Patent

CA 1052278

SUPERSONIC BLADING Abstract of the Disclosure Supersonic rotor blading in an axial-flow fan or compressor employs blades such that shock waves originating on a blade are canceled at the intersection of the wave and the surface of an adjacent blade by virtue of a blade configuration such that the shocks intersect the blade surface at a line of properly oriented change in flow angle of the blade surface. A three-wave system is employed.

157922

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