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Highflyer wrote:
"pintlar" wrote in message ... I was lead to believe the B-52's wing took a negative angle of attack when the engines lost power. For the crew, that is nice to know that this is not true. I think you will find, with ANY airplane, that the angle of attack is solely dependant upon the airspeed and the weight. It would not be expected to change in any way by any power setting, from zero to max. Notice that this is definately NOT true for a powered rotary wing aircraft! :-) Highflyer Highflight Aviation Services Pinckneyville Airport PJY I think you might say *range* of available angle of Attack? Or AOA for straight and level flight? Because at any weight and airspeed, I've always been able to pull the nose up or down - changing the AOA. |
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