The strength and reliability of airplanes depend greatly on the careful design and manufacture of fittings, couplings, and other highly stressed parts. The more important parts of the airplane must be occasionally tested for increased loads and in order to avoid the possibility of defects creeping in during subsequent production. Strength tests are discussed for fittings for wing spar joints, fittings for strut connections, internal bracing, control gear, and landing gear.
Fittings and Other Structural Parts of Airplanes
1923-10-01
Sonstige
Keine Angabe
Englisch
Metal frames and fittings for airplanes
Engineering Index Backfile | 1917
|Engineering Index Backfile | 1942
Structural Safety Measures for Airplanes
Online Contents | 2006
|Structural integrity of future aging airplanes
NTRS | 1991
|Structural Safety Measures for Airplanes
AIAA | 2006
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