Tento projekt byl spolufinancován se státní podporou Technologické agentury ČR v rámci Programu aplikovaného výzkumu a experimentálního vývoje ALFA
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Výzkum užitečný pro společnost.

Project Details

SALI - Software pro stanovení zatížení draku letounu

Project Period: 1. 1. 2013 – 31. 12. 2015

Project Type: grant

Code: TA03010399

Agency: Technologická agentura ČR

Program: Program aplikovaného výzkumu a experimentálního vývoje ALFA

English title
SALI - Software for Airframe Loading Investigation
Type
grant
Keywords

strength analysis; aircraft loading; software

Abstract

The project SALI follows the activities connected with the integrated project
CESAR of the 6th Frame Program of the European Commission.
The software ALAN
was developed in the frame of this project. The goal of the project SALI is
enhancement of versatility of this software, improvement of calculations,
optimization of computational procedures and databases, validation based on
flight tests and first of all preparation for its commercialization. The
important result of the project will be the user's guide and the detailed
analysis of implemented methodology of calculation.
The new software should
replace the very successful software SAVLE which was created in the eighties of
the last century. The architecture of this software does not allow its adaptation
to the new possibilities of computer technology; the accuracy of the dynamic
aircraft model doesn´t correspond to the current knowledge and work with the
program is time-consuming. The consortium of the project partners intends to
utilize their experience with the software SAVLE and ALAN and to create the new
software which has the ambition to become a common software tool for aircraft
certification according to regulation CS-23 and which is accepted by aviation
authorities.
The aim is to create flexible, adaptable and extensible software
which will help to accelerate development work, will be able to archive input
data and calculation results transparently and will improve critical aircraft
loading calculation. It will consequently reduce costs of development and
modification of aircraft, will enhance air traffic safety and will optimize
airframe weight.

Team members
Chudý Peter, doc. Ing., Ph.D., MBA (CM-SFE) – research leader
Dittrich Petr, Ing., Ph.D.
Prustoměrský Milan, Ing. (FIT)
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