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AERODYNAMICS 1. At sea level an aircraft has a minimum landing distance of 2000ft. What would...

AERODYNAMICS

1. At sea level an aircraft has a minimum landing distance of 2000ft. What would be the minimum landing distance of the aircraft at 5000ft density altitude.

2. What is the effect on landing velocity and landing distance if there is a 15% increase of gross weight?(the answer should be given in percents)

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