Structural Analysis of the Lamars Assembly

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Structural Analysis of the Lamars Assembly

Structural Analysis of the Lamars Assembly

M. R. James / G. R. Negaard

This report presents the results of a transient response analysis of the LAMARS primary structure using NASTRAN, level 17.0 (rigid format 9). LAMARS (Large Amplitude Multimode Aerospace Research Simulator) is a five degree-of- freedom motion system composed of a single-place aircraft type cockpit and a display screen at the end of a 30 foot beam. The simulator is used for engineering simulation in order to evaluate flying qualities, flight control system designs and vehicle performance.

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Title :

Structural Analysis of the Lamars Assembly

Contributors:

M. R. James (author) / G. R. Negaard (author)

Publication date :

1981

Size :

114 pages

Type of media :

Report

Type of material :

No indication

Language :

English

Keywords :

Test Facilities & Equipment , Flight simulators , Flight control systems , Computer aided design , Structural analysis , Dynamic response , Degrees of freedom , Lamars(Large amplitude multimode aerospace research simulator) , Nastran computer program

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