• HOME
  • QUIZ
  • CONTACT US
EXAMIANS
  • COMPUTER
  • CURRENT AFFAIRS
  • ENGINEERING
    • Chemical Engineering
    • Civil Engineering
    • Computer Engineering
    • Electrical Engineering
    • Mechanical Engineering
  • ENGLISH GRAMMAR
  • GK
  • GUJARATI MCQ

Machine Design

Machine Design
The ratio of circumferential stress to longitudinal stress in a thin cylinder subjected to an internal pressure is

43832
2
1
4

ANSWER DOWNLOAD EXAMIANS APP

Machine Design
The velocity factor for ordinary cut gears operating at velocities up to 12.5 m/s is equal to

3/(3 + v)
4.5/(4.5 + v)
6/(6 + v)
0.75/(0.75 + √v)

ANSWER DOWNLOAD EXAMIANS APP

Machine Design
The strap end of a connecting rod of steam engine is joined by

Gib of cotter joint
Spigot socket cotter joint
Knuckle joint
Sleeve and cotter joint

ANSWER DOWNLOAD EXAMIANS APP

Machine Design
Deep groove ball bearings are used for

Combined thrust and radial loads at high speed
Radial load at high speed
Heavy thrust load only
Small angular displacement of shafts

ANSWER DOWNLOAD EXAMIANS APP

Machine Design
When an open coiled helical compression spring is subjected to an axial compressive load, the maximum shear stress induced in the wire is (where D = Mean diameter of the spring coil, d = Diameter of the spring wire, K = Wahl's stress factor, and W = Axial compressive load on the spring)

(WD/ πd3) × K
(4WD/ πd3) × K
(8WD/ πd3) × K
(2WD/ πd3) × K

ANSWER DOWNLOAD EXAMIANS APP

Machine Design
The dynamic tooth load is due to

Irregularities in tooth profiles
All of these
Inaccuracies of tooth spacing
Deflections of teeth under load

ANSWER DOWNLOAD EXAMIANS APP
MORE MCQ ON Machine Design

DOWNLOAD APP

  • APPLE
    from app store
  • ANDROID
    from play store

SEARCH

LOGIN HERE


  • GOOGLE

FIND US

  • 1.70K
    FOLLOW US
  • EXAMIANSSTUDY FOR YOUR DREAMS.
  • SUPPORT :SUPPORT EMAIL ACCOUNT : examians@yahoo.com

OTHER WEBSITES

  • GUJARATI MCQ
  • ACCOUNTIANS

QUICK LINKS

  • HOME
  • QUIZ
  • PRIVACY POLICY
  • DISCLAIMER
  • TERMS & CONDITIONS
  • CONTACT US
↑