NOVEL APPROACH TO DESIGN OF LIGHTWEIGHT AND RELIABLE COMPOSITE PRIMARY AIRCRAFT STRUCTURES
The experience of construction of composite primary aircraft structures has approved that the weight decrease for composite aggregates of aircraft in comparison with metallic analogues cannot be obtained within the frames of conventional structures based on stiffened laminated composite skin. One of...
Main Authors: | M. Ch. Zichenkov, I. O. Kondakov, A. N. Shanygin |
---|---|
Format: | Article |
Language: | Russian |
Published: |
Moscow State Technical University of Civil Aviation
2017-01-01
|
Series: | Научный вестник МГТУ ГА |
Subjects: | |
Online Access: | https://avia.mstuca.ru/jour/article/view/994 |
Similar Items
-
The use of probability models for simplified estimates of required reserves reliability control
by: Yu. V. Feshkin
Published: (2016-11-01) -
METHODS OF THE APPROXIMATE ESTIMATIONS OF FATIGUE DURABILITY OF COMPOSITE AIRFRAME COMPONENT TYPICAL ELEMENTS
by: V. E. Strizhius
Published: (2016-11-01) -
Estimation of equivalent stresses and equivalents of the fatigue test programs of airframe composite elements
by: V. E. Strizhius
Published: (2020-04-01) -
Methodology of substantive fatigue life valuation of composite components of aero structure
by: V. E. Strizhius
Published: (2020-04-01) -
Classification of composite materials
by: V A Rogov, et al.
Published: (2012-06-01)