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'Quiet' Mach 6 wind tunnel at Purdue helps shape future aircraft
Perdue University Website ^ | 1-5-2006 | Emil Venere

Posted on 01/09/2006 7:57:05 AM PST by TChris

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1 posted on 01/09/2006 7:57:08 AM PST by TChris
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To: TChris
To help ensure this ultra-clean condition, engineers enlisted the help of an undergraduate student who is a spelunker. The slender student crawled through a 120-foot section of the wind tunnel, wearing a suit like those worn by technicians in clean rooms, and wiped down the inside of the stainless-steel pipe. The pipe is only 18 inches in diameter.

This kid deserves a medal! I get sick just thinking about it!

2 posted on 01/09/2006 8:18:47 AM PST by Paradox (Time to sharpen ole Occam's Razor.)
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To: TChris
The slender student crawled through a 120-foot section of the wind tunnel, wearing a suit like those worn by technicians in clean rooms


3 posted on 01/09/2006 8:23:23 AM PST by ASA Vet (Those who know don't talk, those who talk don't know.)
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To: TChris

This story 'blows'.


4 posted on 01/09/2006 8:35:19 AM PST by YouPosting2Me
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To: zot

Purdue ping


5 posted on 01/09/2006 8:51:07 AM PST by GreyFriar ((3rd Armored Division -- Spearhead))
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To: Paradox

I wonder how big the test section is?


6 posted on 01/09/2006 10:24:47 AM PST by Texas Patriot (Remember.... The Alamo, never forget HOORAHH!!!!!)
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To: YouPosting2Me
This story 'blows'.

Actually it sucks

7 posted on 01/09/2006 10:38:18 AM PST by John O (God Save America (Please))
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To: YouPosting2Me

Didn't you read the story?

This thing doesn't 'blow'....

it actually 'sucks'!


8 posted on 01/09/2006 10:42:55 AM PST by NorthernTraveler
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To: TChris
http://www.sciencedaily.com/releases/2004/05/040512044455.htm

Mimicking Humpback Whale Flippers May Improve Airplane Wing Design

DURHAM, N.C. -- Wind tunnel tests of scale-model humpback whale flippers have revealed that the scalloped, bumpy flipper is a more efficient wing design than is currently used by the aeronautics industry on airplanes. The tests show that bump-ridged flippers do not stall as quickly and produce more lift and less drag than comparably sized sleek flippers.

.....

The sleek flipper performance was similar to a typical airplane wing. But the tubercle flipper exhibited nearly 8 percent better lift properties, and withstood stall at a 40 percent steeper wind angle. The team was particularly surprised to discover that the flipper with tubercles produced as much as 32 percent lower drag than the sleek flipper.

see full article

9 posted on 01/09/2006 12:27:13 PM PST by aimhigh
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To: TChris
The National Aeronautics and Space Administration previously operated a wind tunnel capable of similar performance, but that wind tunnel is not currently in operation.

A long time ago I worked across the street from a superheated helium blowdown tunnel that operated in that range. It exploded one night, throwing extremely hot ceramic "eggs" all over the facility (NASA Ames), setting shrubs afire for blocks around.

10 posted on 01/09/2006 12:45:57 PM PST by sionnsar (†trad-anglican.faithweb.com† | Libs: Celebrate MY diversity! | Iran Azadi 2006 | Is it February yet?)
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To: fnord; phantomworker; sd-joe; Jack Black; TXBSAFH; SouthernBoyupNorth; Ichneumon; ...

Geezer Geek ping.

This is a very low-volume ping list (typically days to weeks between pings).
FReepmail sionnsar if you want on or off this list.

11 posted on 01/09/2006 12:46:27 PM PST by sionnsar (†trad-anglican.faithweb.com† | Libs: Celebrate MY diversity! | Iran Azadi 2006 | Is it February yet?)
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To: sionnsar
A long time ago I worked across the street from a superheated helium blowdown tunnel that operated in that range. It exploded one night, throwing extremely hot ceramic "eggs" all over the facility (NASA Ames), setting shrubs afire for blocks around.

An eggsasperating situation for the engineers, I'm sure.

12 posted on 01/09/2006 12:49:11 PM PST by TChris ("Unless you act, you're going to lose your world." - Mark Steyn)
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To: TChris
The tunnel is relatively inexpensive to operate because each "run" is only about eight seconds. First, air is pumped out of a large tank that is connected to one end of the wind tunnel, creating a vacuum inside the tank. Then a valve is opened between the tank and the wind tunnel, sucking a burst of air through the wind tunnel at high velocity.

The exact method the Nazis used to design the V-2...

13 posted on 01/09/2006 12:56:13 PM PST by null and void (The lesson of the holocaust: if someone says they are going to kill you, pay attention.)
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To: sionnsar

There's also a wind tunnel at the U. Washington where they were "secretly" testing the Sonic Cruiser a while ago.


14 posted on 01/09/2006 12:57:55 PM PST by phantomworker ("Compared to what we ought to be, we are only half awake..." --William James)
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To: sionnsar
Interesting.

The only wind testing I've been directly involved with had been with high rise building and monumental skylight mock-ups, at much, much lower velocities though...;>)

Nontheless impressive when done with water spray.

And while we spec'd the wind tunnel tests of city area models to establish possible wind loads beyond code requirements, I never go the chance to actuall view the tests...damn!

15 posted on 01/09/2006 1:05:44 PM PST by Covenantor
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To: Covenantor

My daughter is a Purdue student.
It is a great university.
I AM AN AMERICAN
http://www.purdue.edu/BANDS/aamb/iamanamericanbg.html


16 posted on 01/09/2006 1:09:44 PM PST by nascarnation
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To: sionnsar

Physical mock ups are outstanding. But in today's world any new design patterns that are developed from it will be computerized for profit before the first design is prototyped. New info concerning that pesky wind problem associated with movement is a good thing.

BUT....Being that I gave up flying when I started making aircraft structural components, I've become steadfast in the belief that if you can't "beam" me from here to there, I ain't going!!! :-)


17 posted on 01/09/2006 1:31:53 PM PST by JoeSixPack1
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To: sionnsar; RightWhale; KevinDavis
The problem they're dealing with is only being addressed in the latter two thirds of the air-flow; -- at the wing edges and engine nacelles, and in the aftermath of the engine and control surface operations.

They will not be able to properly construct their laminar flow-through until they learn to prepare the air before the plane's arrival, for its smooth passage.

If we were speaking of a super-high-speed iceboat, the concept would be obvious. "Ah, yes, we need to heat the ice before the cutting runners arrive, in order to achieve the speed we want."

Exactly. For laminar flow at mach-plus speed, the air has to be pre-heated by lasers focusing at variable distances in front of the craft.

To control it properly, a plane-and-engine-specific pattern will have to be imposed sequentially in front of the plane, so that the air is already expecting it, just as a celebrity can (sometimes) pass unhindered through a thronging crowd.

As far as I know, this idea first saw daylight in my published Science Fiction book of 2004.

18 posted on 01/09/2006 2:14:25 PM PST by NicknamedBob (How can I compete in a world of Cat 5 and wireless when my brain is wired by knob and tube?)
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To: NicknamedBob

The Russian supersonic torpedo must be doing something like this.


19 posted on 01/09/2006 2:18:39 PM PST by RightWhale (pas de lieu, Rhone que nous)
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To: RightWhale

In water, one would need to either superheat the water ahead, or inject a tight column of compressed gas like a drill bit.


20 posted on 01/09/2006 2:22:24 PM PST by NicknamedBob (How can I compete in a world of Cat 5 and wireless when my brain is wired by knob and tube?)
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