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Which of the following is an approach that could rival slats?

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in Aircraft Maintenance by (829k points)
Which of the following is an approach that could rival slats?

(a) Folding wingtips

(b) Carbon fiber fuselage

(c) Flexible wings

(d) Lower takeoff weight

I got this question in my homework.

I need to ask this question from Aircraft Electronics in chapter Aircraft Electronics of Aircraft Maintenance

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Best answer
Correct choice is (c) Flexible wings

For explanation: Flexible wings is a prominent approach that could rival slats. One such project is the X-53 Active Aero elastic Wing, which is a NASA effort.

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