High Speed Flashcards

1
Q

Define Mach Number M

A

The speed of the aircraft divided by the local speed of sound

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2
Q

Define Local Mach Number M L

A

The speed of the aircraft at a particular point divided by the speed of sound at that same particular point

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3
Q

Define Critical Mach Number M CRIT

A

The free stream mach number at which the first local mach number becomes 1

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4
Q

Define the Free Stream Mach Number M FS

A

The mach number aircraft measured at a point sufficiently far from the aircraft as to be unaffected by it

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5
Q

What happens to the CP when an aerofoil accelerates in the transonic range?

A

The formation of the shock wave causes the CP to move rearward

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6
Q

What occurs when an aircraft accelerates through the transonic range?

A

Tuck under (nose down pitch) occurs; this occurs because the aft movement of the CP and the subsequent shockwave causes increased turbulence on the tailplane. Usually overcome by an automatic Mach trim

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7
Q

How could you achieve a higher M CRIT

A

Greater wing sweep and thinner wings

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