Welcome Back

Sign in to your PART66Online account

Forgot password?

Don't have an account? Register here

Q&A Forum

1118 questions found

Module 15. Gas turbine engine

Screech liners in the afterburning jet pipe

  • prevent unstable combustion.
  • prevent cyclic vibrations of large amplitude.
  • acts as noise suppressors.
Jordi asking:

i think the answer is wrong my textbook says that they act as noise suppressors.I quote "These are commonly called as Noise suppression liners or Noise
attenuation mattresses. When installed in the exhaust area these
are also known as Screech liners"

Module 8. Basic aerodynamics

What happens to air flowing at the speed of sound when it enters a converging duct?

  • Velocity increases, pressure and density decreases.
  • Velocity, pressure and density increase.
  • Velocity decreases, pressure and density increase.
rusuvalentin asking:

Why?

Module 8. Basic aerodynamics

If you have an aircraft that is more laterally stable then directionally stable it will tend to

  • bank.
  • slip.
  • skid.
rusuvalentin asking:

Why?

Module 15. Gas turbine engine

What type of intake is one that decreases gradually in area and then increases?

  • Convergent.
  • Convergent / Divergent.
  • Divergent.
Jordi asking:

isnt this divergent only?Why can it be also convergent?I think convergent is the opposite of what it says.

Module 15. Gas turbine engine

Water methanol for cooling is injected into the

  • compressor inlet or outlet.
  • engine hot zone.
  • combustion chamber.
Jordi asking:

why isnt methanol injected into combustion to help with the freezing of water?

We use cookies to keep you signed in and improve your experience. By continuing to use this site, you agree to our Privacy Policy.