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Statement (I) : When a bluff body moves at supersonic speed in still air, an attached shock wave is produced at its nose causing the flow to be subsonic behind the shock plane. Statement (II) : A normal shock always transforms supersonic flow into subsonic flow causing increase in pressure, temperature and entropy.
Consider the following statements: (a) Tellegen’s theorem is applicable to any lumped networks (b) The reciprocity theorem is applicable to linear bilateral networks (c) Thevenin’s theorem is applicable to two - terminal linear active networks (d) Norton’s theorem is applicable to two - terminal linear active networks Which of the above statements are correct?
A subsonic flight has actual inlet pressure recovery of 0.975. Estimate the thrust loss by this subsonic engine.
Which of these processes is involved in slowing down the air inside the subsonic diffuser?
Conical diffuser draft tube consists of conical diffuser with angles of______
Diffuser is installed after turbine where air passes the turbine first then passes through diffuser.
Normal shock diffuser is more efficient than the oblique shock diffuser.
Normal shock diffuser is less efficient than the oblique shock diffuser.
Total pressure loss in a normal shock diffuser is less than the oblique shock diffuser.
Oblique shock diffuser has a better pressure recovery than a normal shock diffuser.