By Arturo O. Cifuentes
The thought of penning this ebook got here up one evening whereas having dinner with Ventura on the Crocodile Cafe in Pasadena. This was once relatively a joint venture, which could have changed into a nightmare with out her aid, encouragement, and services in own desktops. For these kinds of issues, and for tolerating my occasionally single-minded awareness, i'm very thankful to her. i'm additionally greatly indebted to 6 sturdy pals, Paul Burridge, Mladen Chargin, Gary Dilley, Carl Hennrich, Hector Jensen and Mark Miller, who learn the total manuscript of this e-book and made many beneficial feedback. I additionally are looking to thank Burt Alperson for his assistance and suggestion through the instruction of this ebook. ultimately, I thank the dept of Civil Engineering of the collage of Southern California for the help supplied throughout the process this venture, and my scholars of most of these years for asking difficult questions. Contents creation 1 simple MSC/NASTRAN suggestions 2 PARTl Statics challenge 1 7 1. 1 assertion of the matter 7 1. 2 playing cards brought 7 1. three MSC/NASTRAN formula 7 1. four enter information Deck eight 1. five effects eleven challenge 2 27 2. 1 assertion of the matter 27 2. 2 playing cards brought 27 2. three MSC/NASTRAN formula 27 2. four enter facts Deck 27 2. five effects 28 challenge three 37 three. 1 assertion of the matter 37 three. 2 playing cards brought 37 three. three MSC/NASTRAN formula 37 three. four enter info Deck 37 3.
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Extra info for Using MSC/NASTRAN: Statics and Dynamics
The thermal expansion coefficient of the material and the reference temperature have been included in the seventh and eighth fields of the MATI card (a and Tref must be consistent with the units employed in the TEMP cards). In this case the reference temperature is 20°F. This means that the variations in temperature are evaluated using 20°F as a baseline. For example, GRID point 6 is subjected to a change in temperature equal to 20020 = 180 °F. These changes in temperature ultimately determine the thermal Problem 4 49 stresses in the structure; the ambient value of the temperature is, to a certain extent, not important.
0, PAPER TYPE = VELLUM P LOT T E R SIMPLE 2-D TRUSS; STATIC ANALYSIS AXES = +Z,+X,+Y, SYMMETRIC 6, 1988 MSC/NASTRAN 9/ 2/87 PAGE 8 ~ ....... t wnw. SIRPLI 1-. ,.......... 4 Finite element model of a plane truss using rod elements. STATIC ___LVSIS ~ nnw > 4 1-. 5 Deformed and undeformed shape of the truss. LOA. 111 ITATIC AftALYlIS STATIC DEFOR. 2). Assume that the displacements as well as the reactions, stresses, and internal element forces need to be computed. Therefore, additional data recovery requests need to be included in the Case Control Deck.
This output is the result of STRESS = ALL in the Case Control Deck. C H 0 ID PROBLEM,TWO SOL 24 $ WE CAN ALSO PUT COMMENTS HERE IF WE WANT TIME 5 $ THIS IS THE MAX. 1 Executive Control Deck SIMPLE 2-D TRUSS; STATIC ANALYSIS SAME AS PROB. 1 BUT WITH MORE OUTPUT CAS E CON T R 0 L DEC K E C H CARD COUNT 1 TITLE= SIMPLE 2-D TRUSS; STATIC ANALYSIS 2 SUBTITLE= SAME AS PROB. 2 Case Control Deck Problem 2 31 N PUT 2 •• 3 •• BULK D A TAD E C K 5 4 .. 6 7 E C H0 .. $ $ GRID POINTS OF THE MODEL $ GR ID, 1, , 0 .