Originally posted by: Howard
And what causes it to condense? I'm not sure if shock waves are hot, but as pressure increases, the temperature needs to be higher and higher in order for water to stay gaseous.
Originally posted by: 91TTZ
Why do people always assume that the jet is about to break the sound barrier when they see condensation?
This doesn't mean that the jet was going anywhere near the sound barrier. It's just condensation.
I see this misinformation posted all the time.
Have you ever looked at a phase diagram for water???Originally posted by: 91TTZ
Originally posted by: Howard
And what causes it to condense? I'm not sure if shock waves are hot, but as pressure increases, the temperature needs to be higher and higher in order for water to stay gaseous.
The low pressure regions around the aircraft cause it to condense.
Originally posted by: noagname
you do know that pics like that have been out there for years
Originally posted by: buck
Originally posted by: 91TTZ
Why do people always assume that the jet is about to break the sound barrier when they see condensation?
This doesn't mean that the jet was going anywhere near the sound barrier. It's just condensation.
I see this misinformation posted all the time.
Isnt this condensation common right before breaking the sound barrier? (I am not saying its the only time)
*edit*
My comment is referring to the top picture. I am not talking about the little bit that forms on wings and whatnot.
Originally posted by: Howard
Have you ever looked at a phase diagram for water???Originally posted by: 91TTZ
Originally posted by: Howard
And what causes it to condense? I'm not sure if shock waves are hot, but as pressure increases, the temperature needs to be higher and higher in order for water to stay gaseous.
The low pressure regions around the aircraft cause it to condense.
Originally posted by: skyking
Local flow can indeed approach the sound barrier when the aircraft is quite a bit slower.
I see that phenomenon at the propellers of my plane while it is still on the ground accellerating.
Originally posted by: 91TTZ
Originally posted by: skyking
Local flow can indeed approach the sound barrier when the aircraft is quite a bit slower.
I see that phenomenon at the propellers of my plane while it is still on the ground accellerating.
The phenomenon that you're seeing has nothing to do with supersonic flow, though. Your prop isn't going supersonic.
You're just seeing the air condense on the low pressure side of the blade of the prop.
Originally posted by: skyking
Originally posted by: 91TTZ
Originally posted by: skyking
Local flow can indeed approach the sound barrier when the aircraft is quite a bit slower.
I see that phenomenon at the propellers of my plane while it is still on the ground accellerating.
The phenomenon that you're seeing has nothing to do with supersonic flow, though. Your prop isn't going supersonic.
You're just seeing the air condense on the low pressure side of the blade of the prop.
That's true, the bulk of the effect is located mid-span of the blade. Actually, the tips are very close to supersonic speeds.
Listen to a 300HP 520 continental in the Bonanza or C185; it is a horrible racket at 2850 RPM on take off.
It is the limiting factor in propeller driven aircraft. Propellers get enormously inefficient in the transonic region. The reno racers are operating way out of the optimum range, but do it with exorbitant amounts of power and noise
Originally posted by: 91TTZ
Originally posted by: Howard
And what causes it to condense? I'm not sure if shock waves are hot, but as pressure increases, the temperature needs to be higher and higher in order for water to stay gaseous.
The low pressure regions around the aircraft cause it to condense. You can commonly see it above the wings (regardless of what speed it's going), and anywhere else that's a low pressure area. Even if conditions aren't right for the clouds to form above the wings in level flight, a hard turn can cause them to form.
You can also see them on the wings of Formula 1 cars.
The position of the clouds in those pictures tells me that it wasn't going close to the speed of sound.
I've read that pilots in intercepting fighters could hear the Bear from a very long way away, over the noise of their own craft and through the headphones... I suppose the Bear crews must use a great deal of hearing protection, or maybe they're all deaf.Originally posted by: 91TTZ
Originally posted by: skyking
Originally posted by: 91TTZ
Originally posted by: skyking
Local flow can indeed approach the sound barrier when the aircraft is quite a bit slower.
I see that phenomenon at the propellers of my plane while it is still on the ground accellerating.
The phenomenon that you're seeing has nothing to do with supersonic flow, though. Your prop isn't going supersonic.
You're just seeing the air condense on the low pressure side of the blade of the prop.
That's true, the bulk of the effect is located mid-span of the blade. Actually, the tips are very close to supersonic speeds.
Listen to a 300HP 520 continental in the Bonanza or C185; it is a horrible racket at 2850 RPM on take off.
It is the limiting factor in propeller driven aircraft. Propellers get enormously inefficient in the transonic region. The reno racers are operating way out of the optimum range, but do it with exorbitant amounts of power and noise
I remember seeing an episode of Wings of the discovery channel where the air force tried making a fighter (a long time ago) with a supersonic propeller. They succeeded in making it more efficient, but a nasty side effect was that the sound was so horrendous that it made people sick. I hear that the old Soviet Bear bomber also had a horrible drone as its tips were close to supersonic.
Originally posted by: Howard
Umm... a drop in pressure would result in more water evaporating, not condensing.
http://images.encarta.msn.com/xrefmedia/aencmed/targets/illus/cha/T073590A.gif
Originally posted by: Howard
Umm... a drop in pressure would result in more water evaporating, not condensing.
http://images.encarta.msn.com/xrefmedia/aencmed/targets/illus/cha/T073590A.gif