The configuration management requirements for aviation, space and defense organizations
Journal Title: INCAS BULLETIN - Year 2019, Vol 11, Issue 1
Abstract
Certification of the quality management system for aviation, space and defense organizations, according to EN 9100: 2016 / AS 9100D standard requires compliance with the configuration management requirements. This article presents the implementation of Configuration management and documents control throughout the entire life cycle of product realization. Configuration management establishes a language of understanding between the client and the supplier both in predefined relationship (such as Built to Print) and those in which the supplier is given some freedom (such as Built to Spec), described in SR EN 16601-40: 2015 standard.
Authors and Affiliations
Manuela RUSU
Notes regarding the definition and applicability of supercirculation
The term supercirculation refers to an active, fluidic circulation control method used for a variety of aeronautical applications. In particular, this paper refers to supercirculation of entrainment wings. Using experime...
Optimizing Armed Forces Capabilities for Hybrid Warfare – New Challenge for Slovak Armed Forces
The paper deals with the optimization of military capabilities of the Slovak Armed Forces for conducting operations in a hybrid conflict, which represents one of the possible scenarios of irregular warfare. Whereas in th...
Study on aerodynamic resistance to electric rail vehicles generated by the power supply
Improving the traction performance of the electric railway vehicles requires an analysis to reduce their aerodynamic resistance. These vehicles cannot be set in motion without an external power source, which demonstrates...
Low Speed Wind Tunnel Design and Optimization Using Computational Techniques and Experimental Validation
Generally, the experimental aerodynamics is related to wind tunnel experiments. The wind tunnel design topic is very old but the development in computational fluid dynamics led to improvement in the wind tunnel design. T...
Losses and blade tip clearance for a centrifugal compressor
The present paper presents the numerical analysis for a transonic centrifugal compressor using steady state CFD. The blade tip clearance effect over the position of shock waves, tip losses and the performances of the imp...