Question: Integral tanks are ___
Options
A : cavities within the aircraft's airframe itself
B : external tanks needs to be fabricated
C : external tanks required to put in the airframe
D : there is no such type of fuel tank
Airfoil Selection-3 more questions
An airfoil is operated with flow velocity such that the....
An airfoil is such that the drag produced by airfoil....
Determine the corrections or otherwise of the following assertion [A]....
If I want to locate my minimum pressure at 0.5....
Laminar bucket is region where __
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?
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