Axial & Radial Turbine

[@architbansal8923]

Very clearly understable,

[@naviya4403]

Good explanation ❤

[@v.rathod4124]

If U1 and U2 are equal by symmetry, and beta1 and beta2 are also equal by symmetry of the blade, then for axial fans wouldn't outlet velocity be the same as inlet velocity?

[@Prof.raghavendraprasad]

@@v.rathod4124 U1 and U2 depend on hub dia D1 and Blade dia D2 resp. (D2>D1). So your hypothesis fails every time.

[@v.rathod4124]

@@Prof.raghavendraprasad Ah, so is U1 the peripheral velocity and is U2 the base velocity then?

[@engmahmoud3232]

Perfect. Regarding Velocity triangles, How could I express the flow rate for the axial fan based on the geometry, torque and RPM.

[@engmahmoud3232]

Is the velocity triangles for axial fan and axial compressor same exactly or there is difference ?

[@Prof.raghavendraprasad]

@@engmahmoud3232 No...as the design of blade will be different for fan, compressor and for a turbine.

[@srinureguregu4021]

Good explanation

[@Prof.raghavendraprasad]

Thank you

[@ithedimpleboi]

Genious 😍😍

[@Prof.raghavendraprasad]

Thank you very much

[@CamLongThuong]

Tks so much

[@085raveendranathhosamani2]

Thank you

[@nishantakumari1834]

👍🏻