Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight

Howe, D.

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Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight

Howe, D.

URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/4751

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The specimen used in this work represents the load carrying structure of a cambered two spar 60 degree sweptback wing, having closely pitched ribs of large boom area parallel to the line of flight, and thick skins. Continues …

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Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight

Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight

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