Everything yellow and green should be CFP including the outer skin of the aircraft (except the canards). The yellow around the engine section is isolated from the engine by a metal sheet (which is cut open in your last picture, so you only see a part of it).
It says it’s aluminum and titanium.
https://eurofighter.airpower.at/technik-struktur.htm
Judging from these values here:
438 kg → CFP
179 kg → Titanium
174 kg → Alumina
33 kg → Rivets
Even though CFP has much lesser voluemtric mass (1,5 g/cm³) than titanium (4,5 g/cm³) and alumina (2,7 g/cm³) it has a much bigger part of the whole weight of the wing, so its volumetric usage in the wing is about 70-80% (roughly estimated not calculated).
With that constellation the titanium and alumina would be used for the ailerons and the landing gear bay. If the inner structure of the wing were made from alumina and titanium these weights wouldn’t make any sense. So my guess is: Outer skin and inner structure are made from CFP while landing gear bay, some control surfaces and some connection parts (wing to body) are made of metals.
only the outer parts are shown here. The same power frame is not shown. She’s she’s probably all made of metal
it’s metal
I was talking about the wing and the listed weights are for the whole including its inner structure.
I was talking about the wing the whole time lol
I never doubted that the engine bay itself is made from metal as written above.
The TGP sometimes just turns pure white and you need to turn the thermals on and off to fix it
The Gripen wing is attached to the body with ikea bathtub style fittings, and I am not even joking about that. Ever since the Gripen was added with 12G capability I stopped caring about realism in regards to G overloads. @BBCRF
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I will quote myself…
Outer skin and inner structure are made from CFP while landing gear bay, some control surfaces and some connection parts (wing to body) are made of metals.
Clearly more of it is metal, and the Gripen as well;
These aircraft do not show features that are indicative of high sustained G loading.
Congratulations for marking everything I said that would be out of metal…
Outer skin and inner structure are made from CFP while landing gear bay, some control surfaces and some connection parts (wing to body) are made of metals.
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Every plane uses the max airframe limits in WT,m not operating limits…
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That’s your phrase
The Gripen is not intended to do more than 9G once every 1000 flight hours and 12G less often. The Viggen was rated similarly, 9G every 1,000 flight hours but has no overload beyond that. The Gripen is prone to cracks and unlike the Viggen ended up with higher than expected wear/tear IRL.
The Eurofighter design is better than the Gripen, but the aircraft is also much larger and heavier.
I think there was a miscommunication, he contradicted himself in his own statement and it confused everyone. I think we are all on the same page.
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Then read the rest of the sentence where I list the exceptions. Can’t be that complicated…
There is a language barrier, if you say something and then contradict it you will not do yourself any favors. “Everything is yellow”, “except for everything that is yellow and falls under this list”, proceeds to list half the airframe.
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Is there really no concept in other languages like “Everything except [list]”?
This is a known logical contruct in programming languages too so I kind of doubt that.