augmented tube
aircraft powerplant consist of engine, plus inlet and exhaust nozzle.
exhaust from plane
Exhaust Gas Temperature
High performance piston aircraft engines do have valve overlap, just like high performance engines used in land vehicles, and for the same reasons. Listen to the Continental O-470, IO-520, IO-550, even IO-360 at idle (or Lycoming IO-540) and you can hear the same exhaust note quality as a racing car engine.
Most common use is in Exhaust Gas Temperature probes.
its because of micro crystalline ice formation at high altitudes due to exhaust gases (Vapor) from the aircraft engine
The design of the engine intake and exhaust can do a lot to reduce noise levels.
An afterburner is a device in the engine of an aircraft which injects fuel into the exhaust system to increase thrust.
On Lycoming engines the exhaust pipes have a welded steel flange that seats over a copper gasket with 2 studbolts directly onto the outlet port of the engine.
Air intake and exhaust. Air comes into the intake located at the front of the aircraft and exits at the rear of the aircraft. This is such a load of crap! A jet pipe is located at the back of an engine, just after the exhaust! It is connected with a gas tight sealing ring and just before the propelling nozzle. And pipes the exhaust gasses out of the fuselage/Wing... A/C engineer.
General rule: either too much heat or too much pressure. But...fails how ? on what engine and in what aircraft ? Specific questions beget specific answers
A. W. Morley has written: 'Variation of exhaust gas temperature along the tail pipe of a Moth aircraft, and the effect of a simple silencer' 'Aircraft propulsion'