PMB Aerospace

Aerospace Structural Analysis Software

*** NEW!!!! ***

Web access to 48 software!! Run online your jobs! No installation needed.Click here.


Nonuniform, nonhomogeneus composite plate analysis (with longitudinals). BETA version released. Learn more here.

Non linear version under development: Postbuckling analysis of composite shells

48 software

Composite and Metallic stiffened shell analysis

Request your Quotation

Stiffened Isotropic Perforated Plates Elastic Buckling Analysis

simply suported plates with reinforcing ring.



METALLIC FLAT PERFORATED PLATE DATA FOR ANALYSIS

Centered circular hole with circular reinforcement.

Panel Analysis Model Geometry

Job title:


Panel length, a:

Panel width, b:

Following limits apply: d = min(a,b)/2, 1.5<= d/Ro

Outer Radius, Ro:

Following limits apply: 1.2<= Ro/Ri <=4.0

Inner Radius, Ri:


Panel Elastic Modulus, E:

Panel Poison's ratio, nu:

Panel Thickness, t:

Panel Reinforcement Thickness, tr:



BOUNDARY CONDITIONS

Boundary conditions along length edges:

Boundary conditions along width edges:



LOADS

Longitudinal flow, Nx:

Transversal flow, Ny:

Shear flow, Nxy:



Run your job :


It takes 2-3 min to run, please be patient!

Need more computing speed? contact us at sales [at] pmbaerospace.com




You should get these results after running the example.

Panel Analysis Results - static and buckling