Quiz SPL - Page 2 - Principles of Flight (Aeroplane)

The center of pressure is the theoretical point of origin of...	4 Answers
Number 2 in the drawing corresponds to the... See figure (PFA-010) Siehe Anlage 1	4 Answers
Number 3 in the drawing corresponds to the... See figure (PFA-010) Siehe Anlage 1	4 Answers
The angle of attack is the angle between...	4 Answers
The ratio of span and mean chord length is referred to as...	4 Answers
Which point on the aerofoil is represented by number 3? See figure (PFA-009) Siehe Anlage 2	4 Answers
Which point on the aerofoil is represented by number 4? See figure (PFA-009) Siehe Anlage 2	4 Answers
Which point on the aerofoil is represented by number 1? See figure (PFA-009) Siehe Anlage 2	4 Answers
What pattern can be found at the stagnation point?	4 Answers
What pressure pattern can be observed at a lift-generating wing profile at positive angle of attack?	4 Answers

Quiz SPL - Sailplane Pilot License - Principles of Flight (Aeroplane) Page 2