I can imagine this lecture being difficult to follow for certain students, if not familiar at all with the topic. The questions asked at the end reflect this. Language can become a barrier sometimes.
Hi, my name is Igor and I'm a Naval Architect & Marine Engineer from Brazil. I'm a master degree student in ocean engineering and this class helps a lot talking about Structural stability. My reference books are Ship Structural Analysis and Design (2010) from Hughes and Paik, Ultimate Limit State Analysis and Design of Steel Structures (2018) from Paik and the classical book The Theory of Elastic Stability (1961) from Timoshenko and Gere. Thanks for TU Delft from Brazil.
at minute 25:48 he said "the classify profile sections at the same whay" but why are the values of c/t not the same in the beam theory classification section class 4 compered to the plate theory. so why in beam theory its c/t< 15 and in plate theory c/t < 18 ( according to his slides ) as they both are talking about a flange with one free side.
I can imagine this lecture being difficult to follow for certain students, if not familiar at all with the topic. The questions asked at the end reflect this. Language can become a barrier sometimes.
fantastic class thanks
Hi, my name is Igor and I'm a Naval Architect & Marine Engineer from Brazil. I'm a master degree student in ocean engineering and this class helps a lot talking about Structural stability. My reference books are Ship Structural Analysis and Design (2010) from Hughes and Paik, Ultimate Limit State Analysis and Design of Steel Structures (2018) from Paik and the classical book The Theory of Elastic Stability (1961) from Timoshenko and Gere. Thanks for TU Delft from Brazil.
at minute 25:48 he said "the classify profile sections at the same whay" but why are the values of c/t not the same in the beam theory classification section class 4 compered to the plate theory. so why in beam theory its c/t< 15 and in plate theory c/t < 18 ( according to his slides ) as they both are talking about a flange with one free side.
Excellent
Important buckling stiffeners info at minute 22.
Sir, in case of A if all sides are constrained C-C, then how axial load is applied. ist it under external pressure?
Cannot speak properly. Not well prepared