Obiettivo The aim of this project is to produce a computer model capable of predicting the interactional aerodynamic effects between helicopter rotor blades and the fuselage.The general scope of the program was the improvement of methodologies and prediction methods for interactional aerodynamics, in order to provide benefits in the helicopter design phase.The computational methods available to predict isolated helicopter main rotor flow, isolated fuselage flow and rotor/fuselage interaction phenomena were discussed.The experimental activities to generate new data covered a wide spectrum to meet the needs of the code validation process. The tests included:isolated rotor (subscale) in hover and forward flight;fuselage alone;rotor/fuselage (subscale) in hover and forward flight;rotor/fuselage (subscale) in forward flight.Isolated and uncoupled rotor calculations were performed. The different methods used covered a wide range of theoretical approaches, from the simplest momentum theory to the boundary element method with a free wake rotor calculations. The correlations showed that at least a lifting line method with a vortex rotor wake is necessary to simulate correctly the velocity field above the rotor disk.Isolated and uncoupled fuselage calculations were performed using methods. Correlations with the experiment were satisfactory.The combined rotor/fuselage calculation methods typically use a lifting line representation for the rotor with a prescribed wake model and a steady panel method for the fuselage. The calculated results obtained show relatively good agreement with the experiment above the rotor disk for the mean and instantaneous velocities.A global rotorcraft model based on the boundary element method has been formulated and preliminary results have been presented. A panel method representation of the fuselage and of the thick blades isused along with a prescribed rotor wake model. The modelling tools developed in the project need to be improved in order to increase the range of configurations for which they provide reliable calculations.It will commence with a survey to identify and compare the computational methods currently available to European industry and research centres. Experimental campaigns will be carried out using 3 different wind-tunnel test facilities. The test matrix and the most significant measurements for each campaign will be specified, such as the measurements required for CFD purposes. The complete rotor/fuselage interactional aerodynamics problem will be outlined, from the computational point of view, by addressing some intermediate topics: firstly, the isolated rotor and fuselage analysis will be considered; secondly, the uncoupled rotor and fuselage case (the flowfield of the former analysis taking into account the presence of the latter, and vice versa); thirdly, the coupled rotor/fuselage case (combining rotor and fuselage flowfield calculations); and finally, global integrated models. For each topic, the following aspects will be covered: the methods and the algorithms to be assessed, using selected test cases from the updated experimental database; the improvements/enhancements needed for each method and algorithm; and the possible development of new computational models. The final report will provide a specification for the future development of an overall helicopter prediction methodology which will model the interactional aerodynamics effects on the performance of the aircraft. Campo scientifico natural sciencescomputer and information sciencesdatabasesnatural sciencescomputer and information sciencescomputational scienceengineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftrotorcraftengineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaeronautical engineering Programma(i) FP2-AERO 0C - Specific research and technological development programme (EEC) in the field of industrial manufacturing technologies and advanced materials applications (BRITE/EURAM) - Specific activities relating to aeronautics -, 1989-1992 Argomento(i) Data not available Invito a presentare proposte Data not available Meccanismo di finanziamento CSC - Cost-sharing contracts Coordinatore Agusta SpA Contributo UE Nessun dato Indirizzo Via Giovanni Agusta 520 21017 Cascina Costa di Samarate Varese Italia Mostra sulla mappa Costo totale Nessun dato Partecipanti (12) Classifica in ordine alfabetico Classifica per Contributo UE Espandi tutto Riduci tutto Aérospatiale Société Nationale Industrielle SA Francia Contributo UE Nessun dato Indirizzo 37 boulevard de Montmorency 75781 Paris Mostra sulla mappa Costo totale Nessun dato CENTRO ITALIANO RICERCHE AEROSPAZIALI SCPA Italia Contributo UE Nessun dato Indirizzo Via Maiorise 81043 CAPUA Mostra sulla mappa Costo totale Nessun dato EUROCOPTER DEUTSCHLAND GMBH Germania Contributo UE Nessun dato Indirizzo INDUSTRIESTRASSE 4 DONAUWORTH Mostra sulla mappa Collegamenti Sito web Opens in new window Costo totale Nessun dato GERMAN AEROSPACE CENTRE Germania Contributo UE Nessun dato Indirizzo Linder Höhe 51147 KOELN Mostra sulla mappa Collegamenti Sito web Opens in new window Costo totale Nessun dato Institute of Computational Engineering Alfapi SA Grecia Contributo UE Nessun dato Indirizzo 304,Messoghion 15500 Athens Mostra sulla mappa Costo totale Nessun dato LUDWIG-MAXIMILIANS UNIVERSITY OF MUNICH Germania Contributo UE Nessun dato Indirizzo Geschwister-Scholl-Platz 1 80539 MUENCHEN Mostra sulla mappa Costo totale Nessun dato Office National d'Études et de Recherches Aérospatiales (ONERA) Francia Contributo UE Nessun dato Indirizzo 29 avenue de la Division Leclerc 92322 Châtillon Mostra sulla mappa Costo totale Nessun dato Stichting Nationaal Lucht- en Ruimtevaart Laboratorium Paesi Bassi Contributo UE Nessun dato Indirizzo 8300 AD Emmeloord Mostra sulla mappa Costo totale Nessun dato TECHNICAL UNIVERSITY OF DENMARK Danimarca Contributo UE Nessun dato Indirizzo Anker Engelundsvej 1, Building 101 2800 LYNGBY Mostra sulla mappa Costo totale Nessun dato TECHNISCHE UNIVERSITAET BRAUNSCHWEIG Germania Contributo UE Nessun dato Indirizzo POCKELSSTRASSE 14 38106 BRAUNSCHWEIG Mostra sulla mappa Costo totale Nessun dato University of Bristol Regno Unito Contributo UE Nessun dato Indirizzo Senate House Tyndall Avenue BS8 1TH Bristol Mostra sulla mappa Collegamenti Sito web Opens in new window Costo totale Nessun dato WESTLAND HELICOPTERS LTD. 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