A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIES

This model defines the structure and applicability of aero dynamical complex data (up to four dimensions without flap influence which is separate considered) in steady states calculus for different configurations and optional cases (ground effect, asymmetrical propulsion (one of engines out) as well...

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Main Authors: Nicolae APOSTOLESCU, Florentin SPERLEA
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2010-03-01
Series:INCAS Bulletin
Online Access:http://bulletin.incas.ro/files/florentin_sperlea_v2no1_full.pdf
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spelling doaj-b7a7def972824ce69e7203adef3b51a82020-11-25T00:21:27ZengNational Institute for Aerospace Research “Elie Carafoli” - INCASINCAS Bulletin2066-82012247-45282010-03-0121658010.13111/2066-8201.2010.2.1.9A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIESNicolae APOSTOLESCUFlorentin SPERLEAThis model defines the structure and applicability of aero dynamical complex data (up to four dimensions without flap influence which is separate considered) in steady states calculus for different configurations and optional cases (ground effect, asymmetrical propulsion (one of engines out) as well as in dynamic simulations.They user is offered many facilities of data entry, correction and graphical view. The punctual values of dimensional parameters for each coefficient are automaticaly checked for the string strictly increased or decreased specific feature.http://bulletin.incas.ro/files/florentin_sperlea_v2no1_full.pdf
collection DOAJ
language English
format Article
sources DOAJ
author Nicolae APOSTOLESCU
Florentin SPERLEA
spellingShingle Nicolae APOSTOLESCU
Florentin SPERLEA
A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIES
INCAS Bulletin
author_facet Nicolae APOSTOLESCU
Florentin SPERLEA
author_sort Nicolae APOSTOLESCU
title A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIES
title_short A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIES
title_full A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIES
title_fullStr A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIES
title_full_unstemmed A MODEL FOR AERODYNAMICAL DATA STRUCTURE; GRAPHICAL INTERFACE AND USER’S FACILITIES
title_sort model for aerodynamical data structure; graphical interface and user’s facilities
publisher National Institute for Aerospace Research “Elie Carafoli” - INCAS
series INCAS Bulletin
issn 2066-8201
2247-4528
publishDate 2010-03-01
description This model defines the structure and applicability of aero dynamical complex data (up to four dimensions without flap influence which is separate considered) in steady states calculus for different configurations and optional cases (ground effect, asymmetrical propulsion (one of engines out) as well as in dynamic simulations.They user is offered many facilities of data entry, correction and graphical view. The punctual values of dimensional parameters for each coefficient are automaticaly checked for the string strictly increased or decreased specific feature.
url http://bulletin.incas.ro/files/florentin_sperlea_v2no1_full.pdf
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