NDLI: Buclasp 3: a computer program for stresses and buckling of heated composite stiffened panels and other structures, user's manual

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Buclasp 3: a computer program for stresses and buckling of heated composite stiffened panels and other structures, user's manual

Content Provider	NASA Technical Reports Server (NTRS)
Author	Tamekuni, M. Tripp, L. L. Viswanathan, A. V.
Copyright Year	1973
Description	The use of the computer program BUCLASP3 is described. The code is intended for thermal stress and instability analyses of structures such as unidirectionally stiffened panels. There are two types of instability analyses that can be effected by PAINT; (1) thermal buckling, and (2) buckling due to a specified inplane biaxial loading. Any structure that has a constant cross section in one direction, that may be idealized as an assemblage of beam elements and laminated flat and curved plate strip-elements can be analyzed. The two parallel ends of the panel must be simply supported, whereas arbitrary elastic boundary conditions may be imposed along any one or both external longitudinal side. Any variation in the temperature rise (from ambient) through the cross section of a panel is considered in the analyses but it must be assumed that in the longitudinal direction the temperature field is constant. Load distributions for the externally applied inplane biaxial loads are similar in nature to the permissible temperature field.
File Size	4058808
Page Count	231
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19730016168
Archival Resource Key	ark:/13960/t25b4w26d
Language	English
Publisher Date	1973-03-01
Access Restriction	Open
Subject Keyword	Structural Mechanics Panels Stress Analysis Structural Stability Flat Plates Stiffening Laminates Thermal Stresses Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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