High Speed Aerodynamics Flashcards

1
Q

what speed is considered subsonic flow?

A

this is speeds below mach 0.75

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2
Q

what speeds are considered transonic?

A

these are speeds between Mcrit and M1.3

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3
Q

what speed becomes supersonic?

A

these are speeds above M1.3

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4
Q

What happens to all the variables in a normal subsonic shockwave?

A
static pressure - increases
velocity - decreases
temperature - increases
total pressur e- decreases
density - increases
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5
Q

what is MCrit

A

the speed at which at least one portion of the upper surface reaches mach 1

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6
Q

what happens to shockwaves as you start to increase mach number?

A
  • shockwave moves rearwards
  • second shockwave is formed under wing
  • both move rearwards until mach 1 where they are both at the back
  • M1.05 bow wave forms ahead of wing
  • at mach 1.3 the shockwave attaches to the wing
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7
Q

what happens to the shockwave angle as you increase mach number?

A

the shockwave angle becomes more acute the faster that you fly.

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8
Q

what happens to the variables in an oblique shockwave?

A

pressure - increases
velocity - decreases
total pressure - decreases

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9
Q

what happens to Total pressure and velocity in a shockwave?

A

they both decrease

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10
Q

what happens in shockwave compression?

A

temp -increases
total pressure - decreases
density - increases
velocity - decreases

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11
Q

what is high speed buffet?

A

separated airflow from the shockwaves hits the tailplane and acts like turbulence.

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12
Q

what happens in shockwave expansion?

A

temp -decreases
total pressure - increases
density - decreases
velocity - increases

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13
Q

what’s the equation for mach shockwave angle?

A

1/mach no

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14
Q

affect of angle of attack on mcrit?

A

with increase in angle of attack the mcrit value will decrease.

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15
Q

what is a shock stall and why does it occur?

A

loss of lift due to airflow seperation when flying faster than MCRIT

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16
Q

what is mach trim system used for?

A

this is used to counteract mach tuck under.