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Supersonic propellor tips?

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Old 1st September 2006 | 13:52
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Supersonic propellor tips?

Im looking to find oout exactly what happens when propellor tips reach supersonic speeds. After reading books and asking other pilots the only answer I can get is that "bad stuff happens", but no real concise answer.

I presume the shockwave produced from breaking the sound barrier might cause damage to the prop or aircraft itself?
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Old 1st September 2006 | 14:41
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Ronnie, try google. There is a lot of info on this.
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Old 1st September 2006 | 14:44
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From: Too close to Croydon for comfort
The ear splitting rasping noise Harvards and Stearmen and similar types sometimes make is the prop tips going supersonic - I've always believed that pilots try to avoid it causing bad PR around airports rather than because anything catastrophic will eventually happen.

Harvards were banned from Biggin Hill in the 1980s because of the noise.
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Old 1st September 2006 | 14:51
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"Revolutions per minute: For the same propeller diameter, the blade tips travel faster and faster as the rotational speed increases. Eventually, the blade tips become supersonic where shock waves form, drag increases substantially, and efficiency plummets."

http://www.aerospaceweb.org/question...on/q0039.shtml

I haven't come across anything about damage in particular.
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Old 1st September 2006 | 15:41
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From: Yearning for sun and sea
Originally Posted by ronnie3585
Im looking to find oout exactly what happens when propellor tips reach supersonic speeds. After reading books and asking other pilots the only answer I can get is that "bad stuff happens", but no real concise answer.

I presume the shockwave produced from breaking the sound barrier might cause damage to the prop or aircraft itself?
Am I right in thinking that the Grumman Avenger propeller tips on max take off power used to achieve supersonic speeds??
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Old 1st September 2006 | 16:45
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I don't think the tips need to actually go supersonic. Prop bladesa are lifting surfaces like wings, so they will first encounter compressability problems, then local superonic airflow due the speeding up of air over the cambered surface.

End result is mach stall - the blade ceases to produce lift (thrust) on the transonic bits, and so looses efficiency.

SSD
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Old 1st September 2006 | 19:47
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From: Too close to Croydon for comfort
Originally Posted by GANNET FAN
Am I right in thinking that the Grumman Avenger propeller tips on max take off power used to achieve supersonic speeds??
Well, at Flying Legends one year, two Avengers flew past with a Catalina - one was audibly mis-behaving power/pitch-wise and my money was on the Avenger NOT flown by Tony Haigh-Thomas! Sounded magnificent though, rather like one of those 1930s flying movies...
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