Results 101 to 105 of about 124 (105)

Composite material blade with twin longeron and twin box structure having laminated honeycomb sandwich coverings and method of manufacturing same

Composites, 1989
openaire   +1 more source

Strength of Initially Wavy Lattice Columns

AIAA Journal, 1980
exaly  

A method of manufacturing spars, longerons and fuselage beams having a variable H cross-section

2011
INSERRA IMPARATO SABATO, AVAGLIANO LUIGI, CAPASSO LUIGI, D AGOSTINO EMMANUELE, DI TOMMASO LUCA, IAGULLI GIANNI   +5 more
openaire   +3 more sources

Composite patch reinforcement of cracked aircraft upper longeron: analysis and specimen simulationOng, C.L., Chu, R.C., Ko, T.C. and Shen, S.B. Theor. Appl. Fracture Mech. Sept. 1990 14 (1), 13–26

International Journal of Fatigue, 1991
openaire   +1 more source

Etude expérimentale du comportement à la fatigue de longerons avec cornières soudées puis retirées

1996
Peeker, E., Voutaz, B., Kunz, P.
openaire   +1 more source