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Nastran

Known as: Direct Matrix Abstraction Program, Ne/nastran, NX Nastran 
NASTRAN is a finite element analysis (FEA) program that was originally developed for NASA in the late 1960s by Stephen Burns of the University of… 
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Related topics

Related topics

10 relations
Extreme Loading for StructuresFinite element methodHyperSizerList of finite element software packages

Papers overview

Semantic Scholar uses AI to extract papers important to this topic.
Review
2007
Review
2007
Black-box structural optimization of a mechanical component
2005
2005
STRUCTURAL ANALYSIS OF AN EQUIVALENT BOX-WING REPRESENTATION OF SENSORCRAFT JOINED-WING CONFIGURATION FOR HIGH-ALTITUDE, LONG-ENDURANCE (HALE) AIRCRAFT
2004
2004
O rthogonal Maximum Sequence Sensor Placements Algorithms for modal tests , expansion and visibility
After discussing standard requirements on sensor configuration and addressing the issue of non triaxial measurements, the paper… 
2003
2003
SENSOR-CRAFT STRUCTURAL OPTIMIZATION AND ANALYTICAL CERTIFICATION*
A structural and aerodynamic optimization of a composite joined-wing configuration is presented here. The configuration fulfills… 
2000
2000
Finite element simulation of a twin-cam 16-valve cylinder structure
1998
1998
Finite element analysis, design and experiment on solid propellant motors with a stress reliever
1990
1990
Distributed Finite Element Analysis Using a Transputer Network
1972
1972
The NASTRAN User's Manual (Level 15)
The User's manual for the NASA Structural Analysis (NASTRAN) program is presented. The manual contains all information needed to… 
1972
1972
The BANDIT Computer Program for the Reduction of Matrix Bandwidth for NASTRAN
A computer program, BANDIT, is described which was developed for use as a preprocessor to NASTRAN to automatically resequence the… 
1971
1971
NASTRAN - A summary of the functions and capabilities of the NASA structural analysis computer system
Description of general purpose digital computer program /NASTRAN/ for analysis of elastic structures under various loading… 
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