Dazzler
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This was posted by Crobato, a very senior Chinese member renowned for his expert opinions and analysis. His analysis of an article published by Chinese magazine are as follows:
Some of the highlights on the test pilot article.
"The maneuverability has a profound effect on me. This is one extremely nimble plane". He says when you pull the stick on the J-7, you can only pull it gradually so you can hold the proper angle of attack. The radius of turn is wide and the maneuverability is not good. On the FC-1, if you pull the stick, you can pull all the way in and get a very big instantaneous turn rate. Due to a quad Fly-by-wire, turn rate of this fighter is just remarkable. (something we witnessed in squadron induction ceremony)
Then the Chinese pilot asked PAF pilot how JF-17's maneuverability compares with F-16? PAF pilot said jf-17 maneuvers better. Then, PAF pilot asked Chinese pilot (who flew F-16 in UK before) the same question, he said they are probably similar. Then, he also said that this maneuverability is just for when it is horizontal and that F-16 is still slightly better for vertical (climb rate) due to superior T/W ratio. Then he talked about the cockpit with the 1 HUD and 3 MFDs. He said that it's like the ones on Gripen and F-18. The MFD gives pilots a really easy interface to work with. each one has 20 buttons to select different information. This allows the pilot to keep his head on flying the aircraft. Then he talked about how China's cockpit and MFD is much further ahead than the Russian ones and the Russians were surprised.
He says or agrees that the FC-1 has superior horizontal maneuverability over the F-16A (maneuvering in the horizontal plane). However due to inferior thrust to weight ratio, the F-16 still has the advantage on the vertical plane.
Avionics are very advanced and pilot workload is easier than any Chinese or even Russian plane at the moment. When compared to the Su-27, the FC-1's horizontal maneuverability easily holds its own, but the vertical maneuverability is inferior than the Flanker. Again thrust to weight ratio is the reason. The FC-1 cannot compare to the Su-27's ultra maneuverability aspects. He explains something here, which is interesting for people to learn. On a mechanically controlled plane like the J-7, you cannot pull the stick all the way through. At transonic speeds, on a delta winged aircraft, the delta can only use a small angle of attack. Once you pull past that limit, you will lose speed, and with it, lift, and the nose of the aircraft goes down. On a fly by wire plane such as the jf-17, you cannot have this problem because the FBW computer processes the inputs and carefully controls the angle of attack.
Some of the highlights on the test pilot article.
"The maneuverability has a profound effect on me. This is one extremely nimble plane". He says when you pull the stick on the J-7, you can only pull it gradually so you can hold the proper angle of attack. The radius of turn is wide and the maneuverability is not good. On the FC-1, if you pull the stick, you can pull all the way in and get a very big instantaneous turn rate. Due to a quad Fly-by-wire, turn rate of this fighter is just remarkable. (something we witnessed in squadron induction ceremony)
Then the Chinese pilot asked PAF pilot how JF-17's maneuverability compares with F-16? PAF pilot said jf-17 maneuvers better. Then, PAF pilot asked Chinese pilot (who flew F-16 in UK before) the same question, he said they are probably similar. Then, he also said that this maneuverability is just for when it is horizontal and that F-16 is still slightly better for vertical (climb rate) due to superior T/W ratio. Then he talked about the cockpit with the 1 HUD and 3 MFDs. He said that it's like the ones on Gripen and F-18. The MFD gives pilots a really easy interface to work with. each one has 20 buttons to select different information. This allows the pilot to keep his head on flying the aircraft. Then he talked about how China's cockpit and MFD is much further ahead than the Russian ones and the Russians were surprised.
He says or agrees that the FC-1 has superior horizontal maneuverability over the F-16A (maneuvering in the horizontal plane). However due to inferior thrust to weight ratio, the F-16 still has the advantage on the vertical plane.
Avionics are very advanced and pilot workload is easier than any Chinese or even Russian plane at the moment. When compared to the Su-27, the FC-1's horizontal maneuverability easily holds its own, but the vertical maneuverability is inferior than the Flanker. Again thrust to weight ratio is the reason. The FC-1 cannot compare to the Su-27's ultra maneuverability aspects. He explains something here, which is interesting for people to learn. On a mechanically controlled plane like the J-7, you cannot pull the stick all the way through. At transonic speeds, on a delta winged aircraft, the delta can only use a small angle of attack. Once you pull past that limit, you will lose speed, and with it, lift, and the nose of the aircraft goes down. On a fly by wire plane such as the jf-17, you cannot have this problem because the FBW computer processes the inputs and carefully controls the angle of attack.
