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Weapon Engineering Quiz

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Weapon Engineering

Weapon Engineering Quiz

1 / 25

The shock  absorbing   capacity  of a bolt may  be increased by _______  its shank  diameter :-

2 / 25

A knuckle joint can be   used in valve   mechanism  of a reciprocating   engine :-

3 / 25

The efficiency of a riveted joint  is equal to ;-

4 / 25

The description of  tolerance  consist of  _________  parts ;-

5 / 25

Within the airfoil section ,  the represented  graph  is :-

6 / 25

Compressor  increase   velocity of the flow ;-

7 / 25

Which  states has not ratified   the  comprehensive Test ban  treaty  ;-

8 / 25

In the levers  of   first type   , the  mechanical  advantage is   ___________ one :-

9 / 25

Aluminum bronze   contains   5 -  10% aluminium  :-

10 / 25

In order to have   smooth  operation,  the minimum  number  of  teeth  on the smaller   sprocket  , for   moderate   speeds,  should be :-

11 / 25

The project to develop   the   1st  nuclear   weapon  in the world  by  US  is known as :-

12 / 25

The critical speed of a shaft is affected by ;-

13 / 25

The dedendum is  the radial  distance  from the  :-

14 / 25

Russia has planned  to  station its  tactical  nuclear  weapon  in which country ;-

15 / 25

The spring   used in gramophones is ;-

16 / 25

Fuel requirement is not  affected by any factor :-

17 / 25

WMD stand for :-

18 / 25

The piston   pin bearing   in   heavy  duty diesel  engine are :-

19 / 25

Cast  steel   components   do not exhibit  the  effect   of directionality   on mechanical   properties :-

20 / 25

Resilience is  a  ability  of  material  to absorb   energy when  deformed   elasticity ;-

21 / 25

The whole  design philosophy   of an aircraft   is termed as ;-

22 / 25

Wood cannot be used to make  any  part of an   aircraft :-

23 / 25

A  chain drive  transmit  ____________  power  as compared to  belt drive ;-

24 / 25

The allowable  static  stress  for  steel   gears  is  ___________ of the ultimate   tensile  stress ;-

25 / 25

Gun should be located near   to the   centerline  of aircraft ;-

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