J-10 Thread III (Closed to posting)

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challenge

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the magazine just mention F-16,but it did give a hint, "F-16 powered by 13,000kg. engine"
the two foward canard is also make of composite material.the author do admit one minor shortcoming was the engine,it is good,ut not good enough.
 

Pointblank

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the magazine just mention F-16,but it did give a hint, "F-16 powered by 13,000kg. engine"
the two foward canard is also make of composite material.the author do admit one minor shortcoming was the engine,it is good,ut not good enough.

That would probably be a F-16 powered by the Pratt & Whitney F100 engine, which has less thrust than the other option, the General Electric F110 engine, which powers the majority of the USAF F-16 fleet.
 

Infra_Man99

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That would probably be a F-16 powered by the Pratt & Whitney F100 engine, which has less thrust than the other option, the General Electric F110 engine, which powers the majority of the USAF F-16 fleet.

13,000 kg is about 28,660 lb.

From what I have read on the USAF website and other military websites, most F-16s in the US have more or less 28,000 to 29,000 lb-ft of max afterburner thrust, with a thrust to weight ratio of around 6.5:1 to 8.0:1.

That's just the thrust. I don't know the details of the engines performance at various altitudes, maneuvers, and velocities. Then there's procurement cost, maintenance, fuel efficiency, response rate, failure characteristics, reliability, etc. Anyhow, I wouldn't be surprised if the US fighter jet engines were generally superior to Russian equivalents.

I guess the F-16 jets' engines' performance have superior response rate to the J-10A jets' engines, and the former engines have more consistent performance at various speeds and altitudes than the latter engines. This would partly explain why the J-10A has superior turning rate and climbing rate (a combo of superior aerodynamics and fly-by-wire system matched with adequate engine performance), while the F-16 has superior acceleration and takeoff distances (superior engine performance).

I take this info with a grain of salt. I saw a video of a J-10A making a short takeoff that is unmatched by any regular F-16 and F-15 I have seen.
 
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challenge

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it is possible that PLAAF may use pakistan F-16 to flew mock dogfight against J-10A.and the article may ,which I suspect F-16A.
 

Infra_Man99

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it is possible that PLAAF may use pakistan F-16 to flew mock dogfight against J-10A.and the article may ,which I suspect F-16A.

The F-16A has a lot less than 13,000 kg of max thrust (according to
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), and you said the article talked about an F-16 with 13K kg of max thrust, so the article's F-16 should be the F-16C or F-16D (2 seater).

I read the F-16A is a superior VR dogfighter than the later F-16 jets, but the later F-16 jets are vastly superior BVR dogfighters. Apparently, the later F-16 jets acquired advanced electronics (fly-by-wire, avionics, & sensors), additional structural components, and heavier, but more powerful engines. In other words, the later F-16 jets weigh a lot more than the F-16A, so the later F-16 jets' thrust-to-weight ratio may be slightly inferior (F-16D) or about the same (F-16C) or substantially better (F-16E and F-16IN) than the F-16A jets, but their wing loading is inferior and their center-of-gravity relative to their center-of-lift is inferior. Once again, I don't know how these engines perform at various altitudes, velocities, and angles of attack. I also don't know other detailed features of these engines (response rate, efficiency, reliability, etc).

Anyhow, the F-16A has a max initial turn rate of 26 degrees/second and a max sustained turn rate of 18 degrees/second. (Source:
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)

If the above info is true, and if the J-10A does have a max turn rate of 33 degrees/sec (Is this initial or sustained?), then the J-10A is a very agile jet. I read the respective numbers for the Su-27 is 28 degrees/sec and 23 degrees/sec. The Su-35 (or any Su-27 variant with canards) has better low speed agility than the non-canard Su-27 variants, but inferior high speed agility than the non-canard Su-27 variants.

But like I previously said, your source claimed the F-16 has a shorter takeoff distance than the J-10A, but I've seen a video of a standard J-10A making a shorter takeoff than any standard F-16 or F-15 I have seen.
 

tphuang

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hmm, Challenge has a way of understating everything China made with strange articles. But this one I think did come out. but J-10A is definitely up there with the other eurocanards when it comes to ITR and STR. 33 is ITR. I think the take-off for J-10 is 350 m and roll rate is 300 deg/s or something like that. I had a post on this when it first came out and some of the numbers came out. I'm skeptical of the claim that J-10 has longer takeoff than F-16.
 

maozedong

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12月21日,暖暖冬日的南疆大地上,400余名官兵庄严列阵,四架崭新的歼-10战机在金色的阳光下一字排开,广空航空兵某部新机授装接装仪式隆重举行。
据悉,这已是该部五年来第二次整建制换装,此次歼-10飞机的列装,标志着该部所属军区远程制空作战能力的大幅提升,同时也给该部作战体系建设和武器装备建设带来了新的转变。在未来三代战机呈剑形部署的南海一线,该部所属防区内通过主战飞机高低搭配、混合配置,其军事任务中攻防兼备的结构将更加合理完善,应急作战能力将实现质的提高。

the article talk about Guangzhou Military Region an airforce unit receive new J-10, I think its 9 division.
 

Deino

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....

the article talk about Guangzhou Military Region an airforce unit receive new J-10, I think its 9 division.

Yes, You can see the 9. Div's badge in the left corner !

My "problem" is, why Scramble.nl and others say the 9. Div is flying J-10 since about one year ... also some J-10 have been seen there long before and now they received officially only their first four machines.

Deino
 
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