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Archive · dataset · 2025

HIRENASD FEM wing only HEX20

Listed in NASA Data Portal

Description

The finite element model being used by the AePW is based on the model provided at **HIRENASD website** The NASTRAN FEM's using HEXA solid elements and identified as "structured"(str) is the one that will be used. Another exists which uses TETRA elements and is labeled "unstructured"(unstr). The original FEM's as provided on the website had different coordinate systems and are in different units. str = mm unstructured = meters The coordinate systems for each of the FEM are different also.

To facilitate use both FEM's were modified so that the x direction is in the flow direction, y - is out the wing and z is goes from lower surface to upper surface of the wing and the models are in meters. Mode shapes and frequencies were calculated with both FEM's and a frequency comparison is provided. The only model NASA has used is the "str" model.

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Comparisons of the FEM as provided from HIRENASD website with as modified are provided

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Topics

Inferred from text
Aerospace engineering 74%
Provenance · 1 source records, 7 field assertions
SourceKeyLast seenRaw
NASA Data Portal65848b45-5ea4-4706-b958-1ce3f182af908 d agoJSON v1
FieldAssertionExtractorEvidence
concepts[field].anzsrc:group:4001enrichment · data nasa govtaxonomy-embedding@1.1.0title+keywords+description (74%)
created_datesource · data nasa govconnector:data_nasa_gov@1.0.0
descriptionsource · data nasa govconnector:data_nasa_gov@1.0.0/notes
license_textsource · data nasa govconnector:data_nasa_gov@1.0.0
publication_datesource · data nasa govconnector:data_nasa_gov@1.0.0
titlesource · data nasa govconnector:data_nasa_gov@1.0.0/title
updated_datesource · data nasa govconnector:data_nasa_gov@1.0.0