Work done by Fokker company on application of Redux bonding process to composite spar boom construction; comparison between compression strength of booms for which components are either riveted or Redux bonded.
Redux for spars
Aeroplane
Aeroplane ; 83 , n 2143
1952
3 pages
Article (Journal)
English
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TIBKAT | 1928
|NTRS | 1928
|Engineering Index Backfile | 1926
|NTRS | 1926
|Engineering Index Backfile | 1927