onetrack Posted January 24, 2023 Posted January 24, 2023 I'm having some difficulty trying to figure out where they're going to locate the landing gear in that exotic-looking design.
old man emu Posted January 24, 2023 Posted January 24, 2023 That "extra wide wingspan" could cause terminal problems. It's back to the drawing boards for the architects of the Sydney West Airport to redesign the ramps. 1
kgwilson Posted January 24, 2023 Posted January 24, 2023 The landing gear will be in the bump under the struts. This is where most large high wings put them such as the ATR. They will need to be fuel efficient. The thin wings will reduce the capacity up there despite a bit more wingspan. 1 1
facthunter Posted January 24, 2023 Posted January 24, 2023 The strut makes the wing unusually rigid for a modern structure. Nev 1
spenaroo Posted January 24, 2023 Posted January 24, 2023 just nice to see the T tails make a comeback
spenaroo Posted January 24, 2023 Posted January 24, 2023 also it struts..... or an unconventional Bi-plane, as I assume they would produce lift too
facthunter Posted January 26, 2023 Posted January 26, 2023 What's so good about T tails. The B 727 when first test flown had 3 times the anticipated load in the vertical stabiliser and it transfers to the rear pressurised bulk head that had to be replaced in some DC-9 because of cracking. A T tail is also inclined to have tail strikes with early or excessive rate of rotation as there's no ground effect to speak of at that point. It will possibly require some tail (rear fuselage) bump protection . What will be the Mmo M crit of this plane? Sub sonic cruise speeds haven't gone any where for about 50years Where's the fuel going to be stored? There's not much volume in those wings and a very high stress concentration where the strut attaches to the Mainplanes. Nev 1
spenaroo Posted January 26, 2023 Posted January 26, 2023 (edited) 21 hours ago, facthunter said: What's so good about T tails. The B 727 when first test flown had 3 times the anticipated load in the vertical stabiliser and it transfers to the rear pressurised bulk head that had to be replaced in some DC-9 because of cracking. A T tail is also inclined to have tail strikes with early or excessive rate of rotation as there's no ground effect to speak of at that point. It will possibly require some tail (rear fuselage) bump protection . What will be the Mmo M crit of this plane? Sub sonic cruise speeds haven't gone any where for about 50years Where's the fuel going to be stored? There's not much volume in those wings and a very high stress concentration where the strut attaches to the Mainplanes. Nev rule of cool, like the Mooney Edited January 26, 2023 by spenaroo 1
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