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 5ft^2, 4ft^2 and 80ft^2 respectively with Pk as 1, 0.5 and 0.3 for component 1, 2 and 3 respectively.
(a) 31ft^2
(b) 50ft^2
(c) 10ft^2
(d) 4ft
The question was posed to me in my homework.
This key question is from Configuration Layout topic in section Configuration Layout Considerations of Aircraft Design