Question: What is the disadvantage of bladder fuel tank?

Options

A : Loss of available fuel volume

B : Self sealing

C : No loss in fuel volume

D : Thrust loading

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Airfoil Selection-3 more questions

Integral tanks are ___

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 will be the location of maximum camber for NACA....

Which of the following is not the type of fuel....

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....

Aerodynamic Coefficients more Online Exam Quiz

Aerodynamic Forces

Aerodynamics - Lift

Aerodynamics - Parasite (Zero-Lift) Drag and Drag due to Lift

Air Loads

Airfoil Selection-1

Conceptual Design Process

Conceptual Sketch Sizing - Empty-Weight Estimation

Conceptual Sketch Sizing - Fuel-Fraction Estimation-1

Conceptual Sketch Sizing - Fuel-Fraction Estimation-2

Conceptual Sketch Sizing - Takeoff-Weight Buildup