True that, a big part of the reason why the Flanker does not have a similar record is likely to be plain lack of opportunity. Also, some 95% of those 104 kills are opponents which you'd EXPECT the F-15 to outperform - the only victories that were even a contest on paper are a handful of MiG-29s. And even then, half of them (the Serbian airframes) were hardly airworthy at the time, let alone fit for combat against a force that was crushingly superior in numbers, situational awareness and training.chuck4 said:But only in gibberish.
Impressive displays, however only the bluish SU-35 with the red air to air only armament performed a Cobra maneuver once in a level flight. The second display where the aircraft had the asymmetric weapons load showed no such maneuvers.It does not one but TWO tail slides with a highly asymmetrical load totalling north of 5000kg, possibly closer to 5500kg
I didn't claim the Su-30MK performed a Cobra - I just thought it was worth posting as the point that Russian aircraft are normally flown without weapons at airshows (nevermind the fact that the same is true for Western aircraft) keeps getting repeated over and over again. As Churchill put it: "When you have an important point to make, don't try to be subtle or clever. Use a pile driver. Hit the point once. Then come back and hit it again. Then hit it a third time - a tremendous whack."lantinian said:Impressive displays, however only the bluish SU-35 with the red air to air only armament performed a Cobra maneuver once in a level flight. The second display where the aircraft had the asymmetric weapons load showed no such maneuvers.
You can be 100% certain they were dummies. Does it matter though? Their mass, centre of gravity and drag characteristics are designed to match those of the real weapons accurately, so the impact on the aircraft's performance is the same (that's what their real function during actual test flying outside the airshow setting is, after all).lantinian said:I also wonder if air show aircraft are allowed to cary real weapons and if those were mounted on the planes were just mockups or aerodynamic dummies.
chuck4 said:Wouldn't the triangular missile bay under the so called "leading edge extension" on the T-50 act as a sort of tip winglet and inhibit to some degree the formation of tip vortices ? So instead of being true Leading edge extensions optimized to give strong vortices, they would only secondarily generate vortices, sort of like the hard chine on F-22?
Also, I am not entirely sure exactly what LEVCON could do. Has anyone see them deflect upwards? I've only seen them deflect downwards. If they only deflect downwards, then they look to me like an extension of the leading edge flaps on the main wing. If this is true, then when the LEVCON deflect downwards, they permit higher angle of attack without airflow separation over the parts of fuselage above the air intakes. This permit the plane to achieve higher AOA without entering the post stall regime.
EricChase88 said:I asked a few questions over at f-16.net, and some of the posters brought up that the T-50 may have a higher bleed rate than the F-22 in tight turns because apparently, greater wing sweep typically means more AOA needed for a given amount of lift and thus more drag.
Also, T-50 has advanced features like LEVCONs and leading edge root extensions to improve lift, while the F-22 has nothing of the sort. I don't see how F-22 can match the T-50 in maneuvering performance.
EricChase88 said:Although airshow performances does not entirely reflect the plane's aerodynamics in actual combat, the Su-35's demonstrations are a lot more aggressive and shows tighter turns and maneuvers than F-22 demo.
kcran567 said:EricChase88 said:Although airshow performances does not entirely reflect the plane's aerodynamics in actual combat, the Su-35's demonstrations are a lot more aggressive and shows tighter turns and maneuvers than F-22 demo.
Go and look at some more f-22 demos for pete's sake. The thing is doing J-turns, back flips, tail slides, and all sharp, crisp, high energy maneuvers. when the engines are going the plane practically looks weightless during hard maneuvers, and you can see the vortices ripping off the wing edges at a much higher energy than what I've seen of any Pakfa of Flanker demos I've looked at. And I'm being fair, I like the Pakfa and the Flanker.
Machdiamond said:I don't know about the F-22 but when I worked on the F-16 in a previous life, airshow performances always started with full fuel because all it took to burn it all was 7 minutes. Gives you an idea of sea level afterburner fuel flows.
Other than that, I agree with BioLum - this discussion is ridiculous.
chuck4 said:Not much.
In addition, just how much would probably depends on how large the leading edge flaps are compared to the chord of the airfoil. If the LEVCONS act as leading edge flaps for the fuselage, they would seem to be fairly small compare to the chord of the fuselage, furthermore, LEVCON only works on a portion of the fuselage, and that portion is nowhere near an ideal lifting shape, with engine nacelles hanging under it.
Radical said:As a side note, I'm actually surprised that these documents are made publicly available. Why would Sukhoi make the T-50's airframe outline diagrams available to the public?
flanker said:Why did you assume PAK FA and F-22 has same wingspan when we know the correct wingspan of both aircafts?
chuck4 said:flanker said:Why did you assume PAK FA and F-22 has same wingspan when we know the correct wingspan of both aircafts?
Wouldn't make any difference if the area comparison is based on "it looks like".
it will be notEricChase88 said:if the back is modified in the future
flateric said:it will be notEricChase88 said:if the back is modified in the future
EricChase88 said:Dr. Carlo Kopp
have a very thorough and extensive analysis of T-50. It is very insightful. It looks like the T-50 can be as stealthy as F-22 if the back is modified in the future.
I just know. Trust me. (c)EricChase88 said:How do you know? I cant see why not.
TaiidanTomcat said:the most tactful thing I can say about Airpower Australia, is that they have decided on the result before they do the analysis.
flateric said:I just know. Trust me. (c)EricChase88 said:How do you know? I cant see why not.
flateric said:TaiidanTomcat said:the most tactful thing I can say about Airpower Australia, is that they have decided on the result before they do the analysis.
you just start reading, it goes kinda good, good (analysis, analysis) but at the unnoticed moment you feel like that you are reading The Hatter memoirs or front page of Pravda or People's Daily.
Notes/References/Bibliography
More than 40 Russian publications were employed in the preparation of this Technical Report. Due to this large number, and the reality that most redundantly restate the same content, the authors have opted not to list these comprehensively.
The only aircraft built by the United States which can survive in airspace contested by the PAK-FA is the F-22 Raptor, and given the time frame of interest, it is the only design which can be adapted to defeat the PAK-FA.
In basic grand strategy terms, the arrival of the PAK-FA leaves the United States with only one viable option if it intends to remain viable in the global air power game - build enough F-22 Raptors to replace most of the US legacy fighter fleet, and terminate the F-35 Joint Strike Fighter as soon as possible,
There's enough open sources information to say that there will be no redesign you think of.EricChase88 said:So you have inside information? How can you know they won't make big stealth improvements in the future like in Su-35S?