Composite access door
作者： Brian H. Korenaga , Jeffrey F. Stulc , Ian C. Burford , Richard B. Tanner
DOI:
关键词: Composite number 、 Engineering 、 Structural engineering 、 Fastener 、 Interface (computing)
摘要: A method of installing a door in an access opening skin aircraft. composite inner panel is positioned against inside face the skin. outer outside plurality fasteners installed through fastener openings panel. The tightened to form chamfered interface between and
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