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Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions

Karpov, Y. S.

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Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions

Karpov, Y. S.

Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions

Karpov, Y. S.

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Check availability in my library

Order at Subito €

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Document information

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Title:

Structural optimization of composite material for aircraft panels with strength, stability, and deflection restrictions

Contributors:

Karpov, Y. S. (author)

Published in:

STRENGTH OF MATERIALS C/C OF PROBLEMY PROCHNOSTI ; 36 ; 570-581

Publication date:

2004-01-01

Size:

12 pages

ISSN:

Type of media:

Article (Journal)

Type of material:

Print

Language:

English

Classification:

© Metadata Copyright the British Library Board and other contributors. All rights reserved.

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