Higher temperature = higher thermal efficiency.
But you want to adapt your cycle to the circumstances. You can turn the stator blades of one or more of the compressor stages around their axis to some extent, you certainly want to have variable geometry for the engine exhaust in supersonic aircraft, possibly also variable air intakes for higher supersonic aircraft, perhaps auxiliary air intakes for high thrust at low speed. You can have bypass ports to let air escape from the compressor at low thrust.
The true variable engine has variable geometry in the turbine(s) and/or large power off takes. Think also about such exotica as the Ryan XV-5.
aviation week: China is developing 4 high bypassChina Developing Four High-Bypass Turbofans
By Bradley Perrett
Source: Aviation Daily
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May 02, 2013
Credit: ComacChina is developing four high-bypass turbofans, only two of which were previously known. All four have potential military and civil applications.
Work at Shenyang on a high-bypass turbofan in the 30,000 lb. class and suitable for large transport aircraft was already known, along with development of the similarly sized CJ-1000 engine for the C919 commercial aircraft.
But it turns out that there are two such engines from the Shenyang design bureau of Avic Engine: the WS-118 and the SF-A. This was revealed in materials prepared for a May 22-23 conference organized by Galleon (Shanghai) Consulting in association with Avic. The Avic connection means the conference materials can be taken as semi-official.
Both engines from the Shenyang Engine and Design Research Institute are based on fighter-engine cores, just as Western aircraft in the 1970s often used combat cores.
The 26,500-lb.-thrust WS-118 is based on the WS-10A Taihang core, which powers the J-10 and J-11B fighters, according to a document prepared for the China Aerospace Propulsion Technology Summit. Avic Engine’s Shenyang Liming Aero-Engine group is scheduled to begin manufacturing it in 2015.
The WS-118 is a candidate for the Y-20 military airlifter and Comac’s C919 airliner, Galleon reports, although it is likely to be underpowered for the Y-20 and too inefficient for the C919. The same design institute is working on a similar but slightly more powerful turbofan, the 28,700-lb.-thrust SF-A, based on the WS-15 core, reputed to be the engine of the J-20 heavy stealth fighter.
The SF-A has been mentioned previously as a prospective C919 engine. Industry executives also report the existence of an SF-B engine, which may be a version of the SF-A.
Meanwhile, a fourth high-bypass Chinese turbofan is in the works, the smaller WS-12C, using the core of the little-known WS-12 combat engine and intended to power the Comac ARJ21 regional jet, whose only publicly revealed engine until now has been the General Electric CF34-10A. With a thrust of 17,600 lb., the WS-12C is under development by the Chengdu Gas Turbine Research Institute.
Originally to be built by Chengdu Engine, it will be transferred to ACAE, the Avic unit developing the CJ-1000, suggesting the engine has a commercial future, even though sales prospects of the much delayed ARJ21, even with a fairly modern Western turbofan, look increasingly doubtful.
TF engine.