This tutorial demonstrates how to use the load set combination data surface to easily create many load sets or load set combinations in Femap w/ NASTRAN.
What is in this webinar? Static Aeroelastic Trim Analysis The first topic to be covered will be how to set up an aeroelastic trim analysis on an entire aircraft, and how to interpret the results. This will include how to setup a control surface, ...
FEMAP Flutter Analysis Example This example will demonstrate how to create the "Aerodynamic model" and specify some analysis parameters used to perform a flutter analysis using NX Nastran. Topics discussed will be: Create an "Aero Panel" (CAERO1 and ...
Within the Aerospace Engineering community, there is an entire sub-discipline devoted to understanding the dynamics of a system and generating loads (propulsive, inertial, aerodynamic, etc). In smaller companies, engineers often need to wear multiple ...
Introduction This article is written by Ben Names and is a continuation of a previous white paper, “The State of Composite Buckling in NX Nastran,” with some updated findings and conclusions. Earlier I posted a white paper addressing some of the ...