The impulse turbine rotor efficiency will have a maximum value of 0.5 cos 2 Î±, where Î± is the nozzle exit flow angle, if the Options: A . &nbspblades are equiangular B . &nbspblade velocity coefficient is unity C . &nbspblades are equiangular and frictionless D . &nbspblade solidity is 0.65

The

Question

The impulse turbine rotor efficiency will have a maximum value of 0.5 cos² Î±, where Î± is the nozzle exit flow angle, if the

Options:

A . blades are equiangular

B . blade velocity coefficient is unity

C . blades are equiangular and frictionless

D . blade solidity is 0.65

Answer: Option C

Submit Your Solution Below and Earn Points !

Next Question

Chapter 1 - GLOBAL STEEL SCENARIO & INDI Part 1 : (13-04-2024) INDUSTRY AND COMPANY AWARENESS (ICA)

Direction Sense Test Part 1 Reasoning (Hindi)

Chapter 1 - RMHP / OHP / OB & BP Part 1 : (14-02-2024) GPOE

Cube & Cuboid Part 1 Reasoning (Hindi)

Data Interpretation (DI) Basic Concept Reasoning (Hindi)

Counting Figures Part 1 Counting Of Straight Lines Reasoning (Hindi)

Sail E0 free webinar Webinars

Real Numbers Part 7 Class 10 Maths

Real Numbers Part 1 Class 10 Maths

Polynomials Part 1 Class 10 Maths

Chapter 3.1 : Overview of Finance & Acco Chapter 3 : Finance & Accounts SAIL E0 - GFM 2024

Chapter 2.1 : Overview Chapter 2 : Materials Management SAIL E0 - GFM 2024

Chapter 1.1 : Personnel Functions- An ov Chapter 1 : Personnel Management SAIL E0 - GFM 2024

GPOE / GPA Combined 1 Free CBT Mock Test SAIL E0 2024

CBT Mixed Test 1 GPOE/GPA SAIL E0 2024