High Speed Flashcards

1
Q

What is the term used for the speed of sound?

A

Mach 1

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2
Q

What does the speed of sound vary with?

A

Temperature

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3
Q

How do you calculate Mach no. ?

A

Velocity of object(v)/local speed of sound(a)
M=v/a

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4
Q

What is the subsonic speed range?

A

0-0.8 Mach

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5
Q

What is the transonic speed range?

A

0.8-1.2 Mach

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6
Q

What is the transonic speed range?

A

0.8-1.2 Mach

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7
Q

What is the supersonic speed range?

A

1.2-5 Mach

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8
Q

What flow is measured for speed ranges?

A

Compressible flow

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9
Q

Where is subsonic flight used?

A

For most commercial and general aviation flights

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10
Q

Is air compressible or incompressible in subsonic flight?

A

Incompressible

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11
Q

How significant is air density change due to pressure at subsonic flight?

A

Negligible

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12
Q

Is air truly incompressible in subsonic flight?

A

No it’s just negligible so ignored

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13
Q

What is transonic flight?

A

Subsonic and supersonic airflow

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14
Q

What type of shockwave occurs in transonic flight?

A

Normal shcokwaves

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15
Q

What do shockwaves cause in transonic flight?

A

Stability challenges & causes airflow separation from wing
Causes nose down pitch tendency

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16
Q

Define supersonic flight?

A

All speeds on aircraft are greater than the speed of sound

17
Q

What speed is hypersonic?

A

Above Mach 5

18
Q

Where is the shockwaves during supersonic flight?

A

Shockwaves moves to rear and is affixed to trailing edge

19
Q

What happens to pressure and air density during supersonic flight?

A

Slight change in pressure and almost no change in air density observed

20
Q

Can air pressure change without air density changing?

A

Yes

21
Q

Is air compressible in supersonic flight?

A

Yes

22
Q

What compression effects develop during supersonic flight?

A

Reduction in coefficient of lift and an increase in coefficient of drag in the supersonic range

23
Q

How do you calculate Mach no. ?

A

Velocity(true airspeed) / local speed of sound

24
Q

What is critical Mach no. ?

A

Lowest mach no. at which airflow at some point reaches the speed of sound but does not exceed it