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Or buy a Falcon and get both!CapnVegetto said:So, it's basically pick your poison. Fast speeds or short field performance?
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Or buy a Falcon and get both!CapnVegetto said:So, it's basically pick your poison. Fast speeds or short field performance?
SO just what are you getting at???? YOU WANNA MAKE SOMETHIN OF IT PUNK????crzepilot said:Great information people, I think this is the first time the beez nest hasn't been kicked around someway or another, on this website.
Falcon Capt said:Or buy a Falcon and get both!
CapnVegetto said:On a GOOD day, you might get .64 mach out of it. The straight wing is not as aerodynamic, and the faster you get, the more drag it creates, thus making it harder to go faster. A swept wing reduces this effect. As you get faster, you get more efficient. Eventually, around about Mach 1, you enter the transonic zone, and sure enough, the efficiency goes away, until you get past the transonic zone into supersonic speeds. But that's a whole other discussion. The downside to it is the fact that your stall speed is much higher, thus increasing your rotate and Vref speeds, thereby requiring more runway. So, it's basically pick your poison. Fast speeds or short field performance?
Guitar Guy said:Speaking for the Ultra/Encore, cruise speed is noticably greater than 0.64 M. In fact, Mmo on the Ultra is 0.755 M and we do cruise in the 0.72-74 M range pretty routinely.
As for high-speed vs. low-speed performance, remember that's what slats and flaps are designed to help with. Ask someone from the Air Force about the C-17.
bitememesa said:In fact the transonic range can be as low as roughly .80 mach. What we don't realize is that due to the curvature of the wing, swept or straight, we accelerate the air over the wing to create lift. Actually we accelerate the air so fast it goes critical (supersonic) briefly and then creates a shockwave as it decelerates back to normal flow. Depending on the wing's capability in handling this determines our critical mach #. Straight wing, poor ability, swept wing, high ability. This shockwave disrupts the airflow over the aft control surfaces and creates amazing amounts of drag. This is also what gives us some nasty high speed characteristics such as control flutter and mach tuch etc. I'm not sure if the Citation straight wings are mach limited, but the CRJ is at .85. But we have a highly critical wing that's relatively horrible departing on short fields.
It's all a trade off.
And I wouldn't believe it until you held a gun to my head that a swept wing was any structurally stronger than a straight wing. The way wings are designed now anyway, they're put into the airplane in one big piece so design really doesn't matter. Strength is really determined by aspect ratio (ie ~30 on a glider, ~4-5 on an F-16) Try pulling 8gs in your Schweizer someday...