Results 301 to 310 of about 3,933,135 (353)
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2001
Shear loads in an aircraft fuselage will occur as a result of bending and torsion. Yield values under shear are necessary during the design phase since the material should not deform plastically below the limit load. The Metal Volume Fraction (MVF) method for shear yield strength prediction of Glare laminates was investigated.
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Shear loads in an aircraft fuselage will occur as a result of bending and torsion. Yield values under shear are necessary during the design phase since the material should not deform plastically below the limit load. The Metal Volume Fraction (MVF) method for shear yield strength prediction of Glare laminates was investigated.
openaire +1 more source
Estimation of runoff critical shear stress for soil erosion from soil shear strength
Catena, 2004Joel Leonard, G Richard
exaly

