Publication Date:
2016-06-07
Description:
A brazed titanium honeycomb sandwich system for supersonic transport wing cover panels provides the most efficient structure spanwise, chordwise, and loadwise. Flutter testing shows that high wing stiffness is most efficient in a sandwich structure. This structure also provides good thermal insulation if liquid fuel is carried in direct contact with the wing structure in integral fuel tanks.
Keywords:
AIRCRAFT
Type:
NASA. Langley Res. Center Proc. of the Symp. on Welding, Bonding, and Fastening; 21 p
Format:
application/pdf