Dynamic study of the virtual prototype of the IAR-99 SOIM Aircraft

Journal Title: INCAS BULLETIN - Year 2013, Vol 5, Issue 3

Abstract

This paper contains a dynamic study of the IAR-99 SOIM aircraft using ADAMS, multibody dynamic solutions. First, the analysis of the whole airplane is envisaged and then the analysis of the flight control system and the landing gear are considered. The study is performed in the idea of upgrading the IAR-99 aircraft being a continuation of a previous study concerning a flutter analysis [9] of the same aircraft, and will be followed by a paper dedicated to modern tools in the stress analysis of the aeronautical structures. Using ADAMS one can build and test complex virtual prototypes, simulating mechanical systems in a realistic manner, both visually and mathematically which is very useful before developing a real prototype. Engineers can study the dynamics of moving parts and how loads and forces are distributed throughout a complex mechanical system as an airplane. In this way multiple design solutions can be analyzed and evaluated in order to shorten the time and to reduce the cost of a new project.

Authors and Affiliations

Daniela BARAN, Dorin LOZICI-BRINZEI, Simion TATARU

Keywords

Related Articles

Analysis Regarding the Effects of Atmospheric Turbulence on Aircraft Dynamics

This paper will analyze the Gust Load Alleviation (GLA) systems which can be used to reduce the effects of atmospheric turbulences generated by wind gusts on vertical acceleration of aircraft. Their purpose is to reduce...

[b]The participation of romanian universities at the partnership “PEGASUS” - a chance for the aerospace higher education in Romania[/b]

The consolidation process of the European Aerospace Industry has implied a continuous process of cooperation and mergers during the last decades, initially within the national borders, but now increasingly across these b...

Nanostructured zirconia layers as thermal barrier coatings

The coatings obtained by thermal spray are used both as antioxidant and connection materials (e.g. MCrAlY type alloys) as well as thermal barrier coatings (e.g. partially stabilized zirconia oxide with yttria oxide). Thi...

Cessna Citation X Business Aircraft Eigenvalue Stability– Part 1: a New GUI for the LFRs Generation

The aim of “Robustness Analysis” is to assess aircraft stability in the presence of all admissible uncertainties. Models that are able to describe the aircraft dynamics by taking into account all uncertainties over a reg...

Download PDF file
  • EP ID EP156875
  • DOI 10.13111/2066-8201.2013.5.3.1
  • Views 85
  • Downloads 0

How To Cite

Daniela BARAN, Dorin LOZICI-BRINZEI, Simion TATARU (2013). Dynamic study of the virtual prototype of the IAR-99 SOIM Aircraft. INCAS BULLETIN, 5(3), 3-11. https://europub.co.uk/articles/-A-156875