Aeronautical and Aerospace Material and Structural Damages to Failures: Theoretical Concepts
The goal of this paper is to investigate the possible directions of some specified methods for aeronautical and aerospace material and structure effectiveness modeling and optimization. Multioptionality hybrid function uncertainty conditional optimization doctrine application is supposed to be imple...
Saved in:
Main Author: | Andriy Viktorovich Goncharenko |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2018-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2018/4126085 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Nondestructive Damage Evaluation in Ceramic Matrix Composites for Aerospace Applications
by: Konstantinos G. Dassios, et al.
Published: (2013-01-01) -
Design and manufacture of parts and assemblies of aerospace structures made of composite materials in conditions of additive manufacturing
by: A. O. Firsin, et al.
Published: (2024-03-01) -
Sandwich Structured Composites for Aeronautics: Methods of Manufacturing Affecting Some Mechanical Properties
by: Aneta Krzyżak, et al.
Published: (2016-01-01) -
Control of Energy Storage Systems for Aeronautic Applications
by: G. Canciello, et al.
Published: (2017-01-01) -
Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch
by: Nour Chafak Mohamed Ibrahim, et al.
Published: (2018-10-01)