NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
NASTRAN: User's ExperiencesThe application of NASTRAN to a wide variety of static and dynamic structural problems is discussed. The following topics are focused upon: (1) methods of analysis; (2) hydroelastic methods; (3) complete analysis of structures; (4) elements and material studies; (5) critical comparisons with other programs; and (6) pre- and post-processor operations.
Document ID
19770013541
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 3, 2013
Publication Date
October 1, 1976
Subject Category
Structural Mechanics
Report/Patent Number
A-6709
NASA-TM-X-3428
Meeting Information
Meeting: Colloq.
Location: Moffett Field, CA
Country: United States
Start Date: October 5, 1976
End Date: October 6, 1976
Accession Number
77N20485
Funding Number(s)
PROJECT: RTOP 020-02-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19770013556WorkDevelopment, documentation and correlation of a NASTRAN vibration model of the AH-1G helicopter airframe19770013555WorkA finite element-analytical method for modeling a structure in an infinite fluid19770013552WorkA numerically efficient finite element hydroelastic analysis19770013563WorkImplementation on a nonlinear concrete cracking algorithm in NASTRAN19770013542WorkNASA's plans for future NASTRAN capability19770013566WorkNASTRAN used in a production environment19770013567WorkA postprocessor system for the data reduction and post analysis of NASTRAN results19770013544WorkEfficient reanalysis of structures by a direct modification method19770013543WorkOn modeling and the use of the NASTRAN thermal analyzer19770013559WorkThermal and Structural Analysis of Helicopter Transmission Housings Using NASTRAN19770013561WorkThe quarter-point quadratic isoparametric element as a singular element for crack problems19770013553WorkA NASTRAN implementation of the doubly asymptotic approximation for underwater shock response19770013545WorkAutomated fully-stressed design with NASTRAN19770013550WorkA comparison of the two NASTRAN differential stiffness techniques19770013560WorkNASTRAN as an analytical research tool for composite mechanics and composite structures19770013562WorkAddition of higher order plate elements to NASTRAN19770013546WorkApplication of NASTRAN to large deflection supersonic flutter of panels19770013554WorkA summary of NASTRAN fluid/structure interaction capabilities19770013558WorkAnalysis of the Learjet 35/36 Wing and Correlation with Experimental Results19770013565WorkModal seismic analysis of a nuclear power plant control panel and comparison with SAP 419770013549WorkReal eigenvalue analysis in NASTRAN by the tridiagonal reduction (FEER) method19770013564WorkSome applications of the NASTRAN level 16 subsonic flutter analysis capability19770013551WorkDeformations of thick two-material cylinder under axially varying radial pressure19770013557WorkApplication of NASTRAN to large space structures19770013547WorkThermal analyses of the International Ultraviolet Explorer (IUE) scientific instrument using the NASTRAN thermal analyzer (NTA): A general purpose summary19770013548WorkThe GSFC NASTRAN thermal analyzer new capabilities
No Preview Available