H-20 bomber (with H-X, JH-XX)

Quickie

Colonel
Not really, after all DSI is driverless supersonic intake... A flying wing bomber obviously will not be expected to reach supersonic speeds.

So a standard fixed air intake with S ducts should be viable on such an aircraft.

Apparently the DSI has a slightly better performance over the diverter inlet in the subsonic speed. Also, no one knows if the flying wing design would reach near supersonic speed?

The new inlet showed slightly better subsonic specific excess power than a production inlet and that verified the overall system benefits of eliminating the diverter. Test pilots remarked that military power settings and thrust characteristics were very similar to standard production F-16 aircraft with the same General Electric F110-GE-129 engine. Considering the overall goal of the flight test program was to demonstrate the viability of this advanced inlet technology, the results were excellent.
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In any case, the bump can also be considered a required part of the S-duct because of the short distance between the engine inlet and exhaust in the above posted flying wing design.
 

Deino

Lieutenant General
Staff member
Super Moderator
Registered Member
I think the DSI is so far more some sort of artistic licence !
 

FORBIN

Lieutenant General
Registered Member
From Henri K blog, very interesting stuff, main points :


Why a long-range, Strategic Bomber ?

Now that the development of a long-range bomber is no longer a myth, it begs the question: Why such a vector?

In principle, with the modernized H-6K and scope of the KD-20 missiles, the army of the Chinese air already has a substantial strategic projection capability within 5 500km.

This radius covers the whole of the first and second island chain, from India, Southeast Asia, Japan, a northern part of Australia, and of course also of Guam.

So why try to go even further ?

If we now look on a map, it is not difficult to notice until Guam, which is now much of the US forces in the western Pacific, it will only leave the Hawaii and Australia in supporting position of the second line.

First, unlike the US, China has no foot to earth in the Pacific. When the B-2A can ask quietly to Guam, future Chinese bombers unfortunately do not have this privilege.

This will require a platform at least equivalent to the US B-2A, ie with a maximum range of 11 000km, to provide a range of 5 000km. So it would be a platform that will weigh over 150 tonnes at takeoff.

And to cross the first and second island chain in any "peace" without having to be escorted by an armada in the air or sea, the platform must either rely on speed or on discretion. So there is not a lot of possible configurations.

As well as the platform for a range of 5000km exist, it will also develop weapons than 4 000km range.

And to achieve both requires not only political will but also the funding and skills.

...

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taxiya

Brigadier
Registered Member
Good to know...

To 9:30, the general said Chinese Army needs to be able to strike Hawaii
Nothing new nor surprising, he also mentioned other possible targets before and after 9:30 mark. The message is that China must be able to counter-attack any location where an enemy can launch an attack on Chinese coast, no difference than a ICBM flying 10 000 km or a LACM + H-6 combo reaching 5500km. At least one other country on this planet can and is taunting to do it when it see fit.

What do surprise me and maybe others as well is that you seem to understand Chinese very well.o_O
 

taxiya

Brigadier
Registered Member
I come across this article
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where the author says about B-2
In this closeup view you can see an auxiliary inlet below and just in front of each of the engine inlets which removes the turbulent boundary layer air flow before it enters the engine. The removed air is then remixed with the exhaust gases to reduce the temperature signature from the engines and so decrease the stealth bomber's visibility to infra-red tracking equipment.

B2Banking2oClockCloseup2.jpg

My understanding tells me that DSI serves the boundary layer issue. As B-2 design has demonstrated, the issue is not limited to supersonic aircraft. So it is reasonable that a Chinese B-2 equivalent may choose to address this issue with a DSI type of inlet to address the same issue instead of B-2's approach of auxiliary inlet. Remember DSI was in early researching phase when B-2 came out. If Grumman had mature DSI back then, it may have opted DSI on B-2. That is what China is doing after DSI has become an ordinary technology to her.

As others have said the bump can serve as part of the S-duct, making the engine and inlet duct's axis in the same or closer plane, rather than in two planes far away as B-2 does (two vertical planes). This can make the aircraft's center fuselage more compact or thinner, which means smaller cross-section area, less drag, faster and longer range, or same range but smaller airframe therefor smaller RCS.

One thing I want to emphasize is that, don't automatically call any bump a DSI because DSI by its name is supersonic which is distracting to enjoy the bump's full potential. It would be more accurate to call it "bump inlet" which is exactly what Chinese call it "蚌式进气道" literally "mussel inlet".
 
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