DEFINITION OF OPERATING PARAMETERS OUTPUT RANGE OF FUNCTIONAL SUBSYSTEMS HYDRAULIC SYSTEMS OF THE AIRCRAFT
To evaluate the operational tolerance field hydraulic output parameters under various working conditions and the flight stages are mathematical relationships and the results obtained in the environment Mathcad in graphical form.
Main Authors: | M. A. Bobrin, L. G. Klemina, A. N. Kozlov |
---|---|
Format: | Article |
Language: | Russian |
Published: |
Moscow State Technical University of Civil Aviation
2016-11-01
|
Series: | Научный вестник МГТУ ГА |
Subjects: | |
Online Access: | https://avia.mstuca.ru/jour/article/view/4 |
Similar Items
-
DETERMINE THE RANGE OF VARIATION OF THE CONTROL SUBSYSTEM OUTPUT PARAMETERS
by: M. A. Bobrin
Published: (2016-11-01) -
DETERMINATION OF OPERATING FIELDS OF TOLERANCES OF HYDRAULIC SYSTEMS PARAMETERS FOR AIRCRAFT BOARD COMPUTER COMPLEX
by: M. A. Bobrin
Published: (2016-11-01) -
THE EFFICIENCY ANALYSIS OF MULTI-AGENT OPTIMIZATION METHODS OF AIRCRAFT DESIGNS ELEMENTS
by: A. V. Panteleev, et al.
Published: (2019-04-01) -
SYNTHESIS METHOD OF THE FUNCTIONAL STRUCTURE HYDRAULIC SYSTEMS
by: B. K. Grankin, et al.
Published: (2016-11-01) -
MATHEMATICAL MODELING OF PLANE IL-76TD-90VD LANDING IN ANTARCTICA
by: M. S. Kublanov, et al.
Published: (2017-01-01)