ATPL - Airline Transport Pilot license - Principles of Flight Pagina 38

Domande Principles of Flight - ATPL Pagina 38

One disadvantage of wing sweep is the stalling characteristics. At the stall:	4 risposte
An aeroplane has a stall speed of 100 KT at a load factor n = 1. In a turn with a load factor of n = 2, the stall speed is:	4 risposte
When flaps are extended in a straight and level flight at constant IAS, the lift coefficient will eventually:	4 risposte
Given the following aeroplane configurations:1. Clean wing2. Slats only extended3. Flaps only extendedPlace these configurations in order of stall angle of attack:	4 risposte
The use of a slot in the leading edge of the wing enables the aeroplane to fly at a slower speed because:	4 risposte
The formula for the Mach Number is: (a= speed of sound)	4 risposte
In the transonic range the aeroplane characteristics are strongly determined by:	4 risposte
When the air is passing through a shock wave the static temperature will	4 risposte
In the transonic range lift will decrease at the shock stall due to the	4 risposte
The speed range between high- and low speed buffet:	4 risposte

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