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sferrin
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Posted: Jan 03, 2009 - 12:41 AM
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jetblast16 wrote:
Concerning the video: http://www.youtube.com/watch?v=IC_uuynsJsc
I was a personal eye witness to that event and in fact, I was right on the beach
parallel to the Raptor as it pulled into the vertical. There was no question that
the jet was in blower (may be full afterburner) as he rose vertically very
quickly due to the near deafening sound the jet was making. It was LOUD,
that video does not do any justice to that fact. As is typical there, there was
a prevailing South/South Westerly wind such that the jet was actually being
blown North; that is, once the Raptor had gone into basically a pure vertical
attitude, the wings were producing no more lift, while the airframe and structures
made a large wind sail! I watched it drift in a Northerly direction from the wind,
while the twin F119 motors were trying their best to sound like a space shuttle
launch! checksixx is correct in his observations IMO regarding the Raptor's ability
to just drift down vertically, while in full control; it certainly appeared as if the
jet was able to do this (at least for awhile). I am sure that a Raptor with may be
10K or less worth of fuel could maintain a hover in a pure vertical attitude for
sometime with both F119s in maximum afterburner.
the thing that's interesting about it to me is that it was all engine. It popped the nose up and climbed S-L-O-W
Here's a close up of that same climb at the same airshow.
http://www.youtube.com/watch?v=ge9PCGyGXeA
(starts around 0:2 |
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JetTest
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Posted: Jan 03, 2009 - 01:42 AM
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| Yes, to transition from horizontal flight at such an obviously low speed to a vertical climb like that shows extreme power and control, much more than the SU films I've seen. Just imagine what it's real capabilities are. |
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Neno
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Posted: Jan 03, 2009 - 09:35 AM
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checksixx wrote:
sferrin wrote:
mil_hobbyist wrote:
checksixx wrote:
Nope, cannot hang simply on a better than 1-to-1 T/W ratio. It will sink.
Does this have to do with airflow at ultra low speeds? I.e. is there some minimum speed at which it can accelerate vertically?
No, it has to do with Checksixx being wrong.
Lol...now I'm instantly wrong. Doesn't surprise me coming from you.
Anywho, for those who care, I posted a quote from Dozer quite a long time ago in which he was asked about the subject being discussed. He stated that at lower airspeed the engines don't put out the full rating of thrust (I think we all know this already). Further he stated that while the jet would start decending, it was so controlable that he could literally hold the jets nose in the vertical all the way to the ground.
For those who care to know, I'm currently working in Kuwait and don't have a lot of time to respond...which is why i short answered this before. Don't like my answer? Track down Michael 'Dozer' Shower or the former F-22 Demo Pilot Paul 'Max' Moga, who is still at Langley I believe and email them. I personally could care less if anyone here takes my word for it or not.
Cheers - Check
Ok, i understand that limited airflow don't allow to get maximun thrust ftom engines in that condition.
Does is this true for any engine or just for the ones optimized for high speed performance?
Even Su37 or a EF2K wouldn't be able to hang on their A/B ? |
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sferrin
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Posted: Jan 03, 2009 - 05:21 PM
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Neno wrote:
checksixx wrote:
sferrin wrote:
mil_hobbyist wrote:
checksixx wrote:
Nope, cannot hang simply on a better than 1-to-1 T/W ratio. It will sink.
Does this have to do with airflow at ultra low speeds? I.e. is there some minimum speed at which it can accelerate vertically?
No, it has to do with Checksixx being wrong.
Lol...now I'm instantly wrong. Doesn't surprise me coming from you.
Anywho, for those who care, I posted a quote from Dozer quite a long time ago in which he was asked about the subject being discussed. He stated that at lower airspeed the engines don't put out the full rating of thrust (I think we all know this already). Further he stated that while the jet would start decending, it was so controlable that he could literally hold the jets nose in the vertical all the way to the ground.
For those who care to know, I'm currently working in Kuwait and don't have a lot of time to respond...which is why i short answered this before. Don't like my answer? Track down Michael 'Dozer' Shower or the former F-22 Demo Pilot Paul 'Max' Moga, who is still at Langley I believe and email them. I personally could care less if anyone here takes my word for it or not.
Cheers - Check
Ok, i understand that limited airflow don't allow to get maximun thrust ftom engines in that condition.
Does is this true for any engine or just for the ones optimized for high speed performance?
Even Su37 or a EF2K wouldn't be able to hang on their A/B ?
Thing is you don't need maximum thrust. All you need is 1-to-1. F=ma remember. If your engines produces well over 1-to-1 at maximum as the F-22's do then you don't need to be able to get their maximum power. |
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sprstdlyscottsmn
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Posted: Jan 03, 2009 - 05:59 PM
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| Su's have a very hard time with T/W because they are so large and so heavy. The more advanced ones weigh around 20 tons empty. The Raptor on the other hand weighs ~17 tons and have stronger engines. Of course I am not counting fuel weight as these airshow maneuvers do not utilize the 10 tons and 9 tons of fuel that they carry, respectively. Also, dont forget that when hovering you lose the dynamic aspect of thrust so your output is limited to ~80% +- 5% of the rated thrust. the ability of the raptor to sit on its tail relatively motionless, even for just a few seconds before pitching over shows a MASSIVE amount of power and controll available. |
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Tinito_16
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Posted: Jan 03, 2009 - 08:17 PM
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sprstdlyscottsmn wrote:
Su's have a very hard time with T/W because they are so large and so heavy. The more advanced ones weigh around 20 tons empty. The Raptor on the other hand weighs ~17 tons and have stronger engines. Of course I am not counting fuel weight as these airshow maneuvers do not utilize the 10 tons and 9 tons of fuel that they carry, respectively. Also, dont forget that when hovering you lose the dynamic aspect of thrust so your output is limited to ~80% +- 5% of the rated thrust. the ability of the raptor to sit on its tail relatively motionless, even for just a few seconds before pitching over shows a MASSIVE amount of power and controll available.
Exactly. |
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ANYTIMEBABY!
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Posted: Jan 10, 2009 - 01:01 AM
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Amazing how the same power output that is in the blackbird was strapped into the raptor... a fighter.... if the blackbird could fly at confirmed speeds of mk3.2 how can the raptor not achieve 3.5 even if not just a dash...
i would also assume that the raptor flies the airshow routine with more than a 1/4 tank afterall its such a demanding flight profile that its mostly flown in A/B... i could be wrong... is there such a thing as a fuel coservative A/B or do we go for max preformance with in safety design limits? im aware of zone 1 -5 but i would think alot of this flight profile requires full power petal to the metal i mean composite srry...  |
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sprstdlyscottsmn
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Posted: Jan 10, 2009 - 05:09 AM
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| yes but the engine in the SR-71 only made ~20% of the thrust at Mach 3.2, the specially designed inlet produced over HALF the thrust! |
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LordOfBunnies
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Posted: Jan 10, 2009 - 05:59 AM
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ANYTIMEBABY! wrote:
Amazing how the same power output that is in the blackbird was strapped into the raptor... a fighter.... if the blackbird could fly at confirmed speeds of mk3.2 how can the raptor not achieve 3.5 even if not just a dash...
i would also assume that the raptor flies the airshow routine with more than a 1/4 tank afterall its such a demanding flight profile that its mostly flown in A/B... i could be wrong... is there such a thing as a fuel coservative A/B or do we go for max preformance with in safety design limits? im aware of zone 1 -5 but i would think alot of this flight profile requires full power petal to the metal i mean composite srry...
Answer: Drag, drag, drag, drag, drag, and drag, oh and .5*rho*V^2*Cd*A... aka drag.
The SR71 supposedly flew at 80k ft (yeah right, keep going up) and the whole thing was meant to be a lifting body. Also look at the shape, an attempt to keep the minimum frontal area. Cd was also meant to be kept to a minimum so the thing didn't need to have very cambered wings. The speed helped it generate the lift. Needless to say you don't need much angle on a flat plate to keep the 170k lb plane aloft at Mach 3.
If the Raptor were designed to do Mach 3.2 like the SR71, then it wouldn't be able to do much more and it was designed to be a fighter. Admittedly the engineering is much more advanced now so the turning radius wouldn't be the size of a state, well maybe Rhode Island. In designing aircraft, its all about meeting your design goals. The SR71 was meant to be uncatchably fast and take pictures, the missiles and whatnot for it seemed to be an amused afterthought of "Hell... why not?"
The Raptor was designed to be an air supremacy fighter so dash would be nice, but is not an exactly a requirement. Admittedly, it can probably do 2.5+ or better if you don't care about the RAM or the crew chief killing you when you get back.
As for afterburners, they are usually either staged or you can vary the fuel flow so its not a bang-bang control scheme. |
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sprstdlyscottsmn
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Posted: Jan 10, 2009 - 09:40 PM
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| Yeah, that too. |
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Tinito_16
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Posted: Jan 10, 2009 - 10:12 PM
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The difference lies in how fast it can go faster. The F-22 probably has the best acceleration of a plane in it's weight class - and apparently it is comparable to an F-16 I read many times how the chase F-16 had to go into AB to keep up with the Raptor, whether this is due to the Vipers carrying bags is debatable, but anyhow, the plane sure can go. |
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cobzz
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Posted: Jan 11, 2009 - 05:03 AM
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Tinito_16 wrote:
The difference lies in how fast it can go faster. The F-22 probably has the best acceleration of a plane in it's weight class - and apparently it is comparable to an F-16  I read many times how the chase F-16 had to go into AB to keep up with the Raptor, whether this is due to the Vipers carrying bags is debatable, but anyhow, the plane sure can go.
Quote:
Accelerating through Mach in military power in the Raptor feels similar to accelerating in full afterburner in an F-15. The Raptor accelerates in full afterburner in one continuous-speed feed. A slight buffet occurs between about Mach 0.97 and 1.08. After that point and to max speed, the aircraft accelerates smoothly and continuously.
...
The best seat in the house for supercruise is from a chase F-16 or F-15. Remember, we fly both these chase jets with just a centerline fuel tank to give them a fighting chance to play with the Raptor. Still, the F-22 usually leaves these aerodynamically “slick” chase airplanes in the dust. The F100-110, -129, and -229-powered F-16s don’t fall very far behind the Raptor in the initial acceleration through Mach. But the race is really no contest at the higher Mach numbers and once on cruise conditions. Nothing can sustain supersonic conditions with the persistence of a Raptor. Load those chase F-16s and F-15s with combat-representative stores and they would not stay with the Raptor during acceleration or sustained cruise.
http://www.codeonemagazine.com/archives ... f22_1.html |
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sprstdlyscottsmn
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Posted: Jan 12, 2009 - 04:00 AM
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| yeah the F-35 and F-22 are powerhouses in operational terms. |
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ANYTIMEBABY!
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Posted: Jan 12, 2009 - 06:35 PM
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| my question is in the thrust to weight category the f-22 slaughters the blackbird, i understand the inlet theory on sr and egt to sustain speed what i dont understand is on paper i would think a raptor should easily turn 3.5 at altitude if not more only for a very limited duration do to egt and outer surface temps. your thoughts please/.... |
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LordOfBunnies
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Posted: Jan 12, 2009 - 07:11 PM
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Not necessarily man. Drag and how things interact at speed affect things a lot. When people quote a Cd for an aircraft they're usually quoting the Cd at a given Reynolds Number or a range where it plateaus. Get the Raptor going fast enough and I'm pretty sure you'll get some gnarly shock-shock interaction. God forbid the thing hit some type 3 or typer for S-S because that'll burn a hole right through it. If you start having shocks intersect things that they're not supposed to you could start damaging the airframe and the drag would skyrocket. The most likely occurance of this would be the nose shock hitting the wingtips.
The answer is NEVER simple in aerodynamics... ever. Nothing so simple as the thrust-weight being better.. truth be told (thrust-drag)/weight is a MUCH more telling stat and that one varies a lot. |
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