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-   -   How STRONG is a 757 ? (https://www.pprune.org/tech-log/525616-how-strong-757-a.html)

Stan Woolley 15th October 2013 08:50

How STRONG is a 757 ?
 
What would it be like at 500kts indicated,low level in a B757 ?

And being around 150kts above Vne,what are the chances of breaking up ? (Assuming you're being gentle on the G - or not?)

What do the boeing test pilots do as a matter of course ? (Indicated)

What is the fastest a Boeing has ever flown and survived ?

PeePeerune 15th October 2013 08:59

Why?.

And why a 757 in particular?.

Not being awkward, just interested in the reasons.

Clandestino 15th October 2013 09:03

Twelve years have passed and folks still don't give up.

GlueBall 15th October 2013 09:06

Don't know about the B757, but the DC-8 had "survived" Mach-1

The DC-8 Supersonic Flight

Dufo 15th October 2013 09:08

Let's calculate dynamic pressure for max design speed and 500 kts indicated at sea level in standard conditions.

At 350 KIAS it is 3.11 psi
At 500 KIAS it is 6.34 psi
; which is more than a double

I would say this is above elastic modulus ((design x 1,5) x 1,15 if I remember correctly) for a structure of this type and permanent damage would occur.

Stan Woolley 15th October 2013 09:19

Clandestino

You're right ,I was reading about 9/11.

I also flew the 757/767 and got to thinking what it would be like at 500kts.

Have you anything useful to say ?

Dufo

Thanks. It might be permanently out of service but would a critical bit break off ? I think it would be noisy :eek:

jimjim1 15th October 2013 09:47

DC8 laundry moment
 
Glueball mentioned


The DC-8 Supersonic Flight
Thanks, well worth a read.

It seems to have been not entirely without incident.

Supersonic flight was achieved in a 20 degree dive.

"however the initial application of full up elevator did not appear to produce any noticeable change in the load factor"

They recovered by using the pitch trim. All moving tail trim? Reading between the lines I sort of guess that this was expected really - but still.

"A severe rudder pedal "buzz" was apparent ... from the oscillograph records ... The rudder control tab maximum movement was recorded as 21.3 degrees double amplitude, at a frequency of approximately 28 CPS."

Not sure what "double amplitude" means but it is still a large movement.

Clandestino 15th October 2013 10:07


Have you anything useful to say ?
1. If you are planning on totalizing your aeroplane at the end of the high speed low pass, there is no point in worrying about long term effects of busting maximum demonstrated speed.

2. this was discussed many times at length here by folks who know a lot about certification testing. Conclusion was it was quite possible for 757 to reach 500 kt practically undamaged. That didn't deter conspiracy theorists, though and it would be even worse if some Buck Rogers wannabe imagines that means he can go through Vmo without consequences.

3. you might find more receptive audience at sites with black background and banners screaming about government keeping us in dark.


I would say this is above elastic modulus ((design x 1,5) x 1,15 if I remember correctly) for a structure of this type and permanent damage would occur.
True only if permanent damage occurs at speed needed to be demonstrated for certification+1kt. In real life you test to requirement and don't care whether your radome collapses or windshield busts or leading edge curls down at that speed plus one or plus fifty. There is such a ting as the overbuilt aeroplane.

cockney steve 15th October 2013 10:11


Not sure what "double amplitude" means but it is still a large movement
Either side of neutral? IE 21.3 * left and the same right, total oscillation excursion =42.6 ?

OutsideCAS 15th October 2013 12:19

Hitting a bird at low level might be a little interesting around the 500kts mark.....

DozyWannabe 15th October 2013 13:42

Added to which, a 757 on a low pass at full chat doesn't sound like you might expect it to - those RB211s make some serious noise!


She acquired the nickname "Mighty" because she was considerably over-powered compared to other types - those engines were originally designed for the much larger and heavier L-1011 TriStar. The RNZAF (see video) have become well-known for displaying their 757s as handling almost like fighters.

Stan Woolley 15th October 2013 13:54

Actually I was thinking about the wind noise in the cockpit when I said it would be loud.

What a great sound & low pass !

It makes a distinctive sound when you press TOGA on take -off. Can't remember similar - maybe the A320 ? Can't imagine that wheezy old trout making the same noise as the Mighty 757 ! ( No offence ) :ok:

DozyWannabe 15th October 2013 14:12


Originally Posted by Stan Woolley (Post 8100182)
It makes a distinctive sound when you press TOGA on take -off. Can't remember similar - maybe the A320 ? Can't imagine that wheezy old trout making the same noise as the Mighty 757 ! ( No offence ) :ok:

Oh, the A320 can be spectacular in her own way, but one thing she isn't is overpowered - she was designed as a pure short-haul type, whereas the B757 was designed for medium-haul, and with the coming of ETOPS has even been used as a long-haul type in her later years. The 757 is definitely one of my favourites of the B types, but the things that made her mighty also made her less economical to run in most use cases as time passed.

flyingchanges 15th October 2013 15:38

That is still the best flyby ever.

DozyWannabe 15th October 2013 17:44


Originally Posted by flyingchanges (Post 8100400)
That is still the best flyby ever.

Oh, I dunno - I suspect the VC-10 at White Waltham edges it:

http://www.abpic.co.uk/images/images/1028300M.jpg

Alas there is no film or video of that one extant.

doubleu-anker 15th October 2013 18:38

Ah the DC 8. They don't make planes like that anymore! Nor the 707 or VC10 for that matter.

As for going supersonic, they were probably lucky to have got away with it. Due to the rapid and large C of P change, a fully flying tail plane is necessary. Using pitch trim was the next best thing, albeit slow, for longitudinal control.

DozyWannabe 15th October 2013 18:55


Originally Posted by doubleu-anker (Post 8100642)
They don't make planes like that anymore! Nor the 707 or VC10 for that matter.

Actually, Airbus have taken a leaf out of the VC-10 book when to comes to attaching the main gear to the A350XWB:

Pictures: Airbus adopts Vickers VC10 landing gear concept for A350 XWB

Anyways - sorry - back on-topic!

Ozlander1 15th October 2013 19:43

They took a B-52 supersonic in level flight. Bent the wings. :=

tdracer 15th October 2013 20:00

I saw flight test data from the 747-8 flutter testing at Mach 0.98 to 0.99.

Really plays havoc with some of the sensors.....

KRviator 15th October 2013 22:33

Didn't that China Airlines 747SP get close to, or exceed, Mach 1 during its upset, they just didn't have the DFDR data to prove it?

Iv'e got a book somewhere that claims they probably exceeded the speed of sound but the flight recorder wasn't working during the periods it would have - convenient?


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