Question: Which of the following is not the type of fuel tank?
Options
A : Flap
B : Integral
C : Bladder
D : Discrete
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Airfoil Selection-3 more questions
Let's consider we need to design supersonic aircraft then, which....
Location of aerodynamic centre for low speed airfoil is __
The maximum lift co-efficient for NACA 19584 (chord=2.5m) airfoil is__
What is the disadvantage of bladder fuel tank?
What will be the location of maximum camber for NACA....
For a typical jet following diagram is presented. What should....
If design is carried out in CAD software then what....
The Configuration layout is revised after optimization and experiences number....
The design take-off gross weight of aircraft is given by....
The three view drawing which shows arrangements of parts during....
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