Configuration Layout - Vulnerability Considerations Online Exam Quiz
Configuration Layout - Vulnerability Considerations GK Quiz. Question and Answers related to Configuration Layout - Vulnerability Considerations. MCQ (Multiple Choice Questions with answers about Configuration Layout - Vulnerability Considerations
A firewall should be provided for vulnerability consideration.
Options
A : TRUE
B : FALSE
C : -
D : -
A wing is to be loft with span as 2m and reference area of wing is 4m2. If we want to design the wing with taper ratio of 0.6 then what will be the value of tip chord?
Options
A : 2.5m
B : 2.50m
C : 2.65m
D : 25.6m
An aircraft component has presented area 6 ft2 with Pk as 1.0. Find vulnerable area.
Options
A : 6ft2
B : 82ft2
C : 7ft2
D : 72ft2
Consider below wing. Calculate the value of span of wing marked by '?'.^
Options
A : 3.3m
B : 6.66m
C : 3.36m
D : 6.96m
If an aircraft has three components which can be considered as vulnerable components then, evaluate total vulnerable area. Given area of component 1, 2 and 3 are 5ft2, 4ft2 and 80ft2 respectively with Pk as 1, 0.5 and 0.3 for component 1, 2 and 3 respectively.
Options
A : 31ft2
B : 50ft2
C : 10ft2
D : 4ft
In order to improve vulnerability consideration, we can use ___
Options
A : redundant components
B : high lift device
C : vortex generator
D : we cannot improve it
Term marked by '?' in diagram is __^
Options
A : tip chord
B : root chord
C : thrust
D : lift
We can improve vulnerability by ___
Options
A : avoiding fuel tanks near to the engine
B : placing fuel tanks on the engine
C : placing fuel tanks inside the engine
D : placing fuel tanks at any location
Aerodynamic Coefficients more Online Exam Quiz
Configuration Layout - Conic Lofting
Configuration Layout - Crashworthiness Considerations
Configuration Layout - Maintainability Considerations
Configuration Layout - Producibility Considerations
Configuration Layout - Structural Considerations
Configuration Layout - Wetted Area and Volume Determination
Configuration Layout - Wing/Tail Layout and Loft-1
Configuration Layout - Wing/Tail Layout and Loft-2
Configuration Layout Considerations - Aural Signature
Configuration Layout Considerations - Infrared Detectability