The diagram shows the parameter X versus TAS. If a horizontal flight is considered the axis X shows4
risposte
On a swept wing aeroplane at low airspeed, the 'pitch up' phenomenon:4
risposte
On a wing fitted with a 'Fowler' type trailing edge flap, the 'Full extended' position will produce:4
risposte
The function of the slot between an extended slat and the leading edge of the wing is to:4
risposte
What increases the stalling angle of attack ? Use of:4
risposte
A slat will:4
risposte
To be able to predict compressibility effects you have to determine the:4
risposte
'Tuck under' is caused by (i) which movement of the centre of pressure of the wing and (ii) which change of the downwash angle at the location of the stabilizer.4
risposte
Air passes a normal shock wave. Which of the following statements is correct?4
risposte
When the air has passed through a normal shock wave the Mach number is4
risposte