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brian whatcott wrote:
/snip/ For instance, how does your ASI indicate at 90 deg AoA ? If an airframe is designed for 1.5 (the design factor) times limit load (often 4 g) then if it is pulled with a force exceeding this, at high AoA, wing breakage is guaranteed. Sincerely Brian W I received a private note that mentioned that gliders may well be built to 6+g limit loads and that parachutes are not mandatory - with some notable exceptions. Where DO I get my preconceptions? :-) Brian W |
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