Interface thermal conductance of twenty-seven riveted aircraft joints / Martin E. Barzelay and George F. Holloway.

Twenty-seven structural joint specimens of 2024-T3 and 2024-T4 aluminum alloy consisting of a T-stringer riveted to a 10- by 10-inch skin surface were tested under simulated aerodynamic heating with no external loading applied. Interface thermal conductance was determined from local transient -tempe...

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Bibliographic Details
Main Author: Barzelay, Martin E.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Holloway, George F.
Format: Government Document Book
Language:English
Published: Washington : National Advisory Committee for Aeronautics, [1957]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3991.
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Call Number: Y 3.N 21/5:6/3991
Y 3.N 21/5:6/3991 Available Place a Hold