Configuration Layout Considerations - Visual Detectability Online Exam Quiz
Configuration Layout Considerations - Visual Detectability GK Quiz. Question and Answers related to Configuration Layout Considerations - Visual Detectability. MCQ (Multiple Choice Questions with answers about Configuration Layout Considerations - Visual Detectability
A. Typical aircraft will have lighter colors at lower surface.^ R. The background lookup angle is sky.
Options
A : Both [A] and [R] are true and [R] is the correct reason for [A]
B : Both [A] and [R] are true but [R] is not the correct reason for [A]
C : Both [A] and [R] are false
D : [A] is false but [R] is true
An observer is observing in an aircraft from distance of 2400 feet. If size of the aircraft can be given as 24000 feet then, what will be the simplified value of visual angle in minutes of arc? Consider all simplified environment and ideal conditions.
Options
A : 34380
B : 3438
C : 343
D : 34
Camouflage patterns for sky background will include __
Options
A : dirty blue-grey
B : clean red
C : clean pink
D : dirty red always
For ground background, camouflage paint scheme consists __
Options
A : mottled grey green
B : mottled white
C : black and red
D : yellow and red only
Higher contrast between different parts of aircraft will ___
Options
A : increase detectability
B : decrease
C : increases twice times always
D : always decreases by two units
If my aircraft has luminance of 10 unit and is designed to operate in background which has luminance of 8 unit then, what will be the approximate value of contrast?
Options
A : 0.25 unit
B : 1.25
C : 5.25unit
D : 5.26
Positioning of the propeller should be such that ___
Options
A : blade will not strike anyone if they fly off
B : blade should fly off during flight
C : it is always near to cabin
D : the blades will strike the engine
Typically, in a passenger aircraft fuel is not located in the fuselage.
Options
A : TRUE
B : FALSE
C : -
D : -
What do you mean by crashworthiness?
Options
A : Capability of structure to protect against impacts and crash loads
B : Capability of an aircraft to stay in cruise
C : Vulnerability to radar detection
D : Special aerodynamic lift improvement
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