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But we (or at least I) am NOT talking about "stall buffet"...There is a point where, due to increasing angle of attack, airflow over the wing goes supersonic, creates a shock wave (more accurately probably an expansion wave) that causes buffet...it's not a stall...depending up on the airplane, you may or may not be able to hold altitude, and you may or may not be able to increase power to fly out of it.Bjammin said:I can buy that, but again we have to be talking when there is only a few knots between stall and mach buffet. I'm sure this only happpens ABOVE the max altitude for the airplane. Except for the U-2.
Depends on the airplane...for a Falcon 10 it is...for a Citation it's not...for a Beechjet it's about right for the climb.Bjammin said:Mach .69 seems like way to low of an airspeed.
Again, it depends on the airplane...I've never seen it in the Hawker, although we do have charts for it. The airplane just becomes a serious slug long before you get to that speed/AOA (still well above "stall") that I've never been tempted to get close.Bjammin said:At FL400 (Max is FL410) I don't get any buffet above the correct AOA for stall buffet and this correlates to a specifc speed at a certain weight. I am usually paying attention to AOA here and not trying to get a specific speed or mach number. On my next functional check flight I will get these numbers for you.
As I said, if your theory were correct for all cases I would expect buffet (from the low speed condition supersonic flow) at an angle of attack less then that for actual low speed stall buffet and I don't experience that.