Development of Wing Aero-Structural Analysis Models and Optimization Survey for the NASA Common Research Model

A Publication, Structural Efficiency - 11 years, 1 month ago

Shared By: JAMES MOORE

Development of a generic wingbox finite element model set based on the NASA Common Research model (CRM) was undertaken to examine fundamental structural dynamics with ...

Common Research Model Wingbox Finite Element Models (V12, V14, V15)

A Publication, Structural Efficiency - 11 years, 2 months ago

Shared By: JAMES MOORE

Several semi-span Wingbox structures were developed based on the CRM OML (outer mold line) loft provided by LaRC-SFW and contains combinations of explicitly modeled shell ...

CRM CONVENTIONAL BASELINE UPDATE

A Publication, Structural Efficiency - 12 years ago

Shared By: JAMES MOORE

PRSEUS LOADSET REPORT-BWB

A Publication, Structural Efficiency - 12 years, 4 months ago

Shared By: JAMES MOORE

Damage Arresting Composites for Shaped Vehicles. PART 25 LOAD SET FOR 4-500K GTOW AIRCRAFT