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Nastran Dmap Fuzzy Structures Analysis: Summary of Research
| AUTHOR | Administration (Nasa), National Aeronaut |
| PUBLISHER | Createspace Independent Publishing Platform (06/19/2018) |
| PRODUCT TYPE | Paperback (Paperback) |
Description
The main proposed tasks of Cooperative Agreement NCC1-382 were: (1) developing MSC/NASTRAN DMAP language scripts to implement the Soize fuzzy structures approach for modeling the dynamics of complex structures; (2) benchmarking the results of the new code to those for a cantilevered beam in the literature; and (3) testing and validating the new code by comparing the fuzzy structures results to NASA Langley experimental and conventional finite element results for two model test structures representative of aircraft fuselage sidewall construction: (A) a small aluminum test panel (SLP, single longeron panel) with a single longitudinal stringer attached with bolts; and (B) a 47 by 72 inch flat aluminum fuselage panel (AFP, aluminum fuselage panel) including six longitudinal stringers and four frame stiffeners attached with rivets. Sparrow, Victor W. Langley Research Center
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Product Format
Product Details
ISBN-13:
9781721502035
ISBN-10:
1721502033
Binding:
Paperback or Softback (Trade Paperback (Us))
Content Language:
English
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Page Count:
30
Carton Quantity:
136
Product Dimensions:
8.50 x 0.06 x 11.00 inches
Weight:
0.21 pound(s)
Country of Origin:
US
Subject Information
BISAC Categories
Reference | Research
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The main proposed tasks of Cooperative Agreement NCC1-382 were: (1) developing MSC/NASTRAN DMAP language scripts to implement the Soize fuzzy structures approach for modeling the dynamics of complex structures; (2) benchmarking the results of the new code to those for a cantilevered beam in the literature; and (3) testing and validating the new code by comparing the fuzzy structures results to NASA Langley experimental and conventional finite element results for two model test structures representative of aircraft fuselage sidewall construction: (A) a small aluminum test panel (SLP, single longeron panel) with a single longitudinal stringer attached with bolts; and (B) a 47 by 72 inch flat aluminum fuselage panel (AFP, aluminum fuselage panel) including six longitudinal stringers and four frame stiffeners attached with rivets. Sparrow, Victor W. Langley Research Center
Show More