TFAST
Transition Location Effect on Shock Wave Boundary Layer Interaction
| Coordinatore | INSTYTUT MASZYN PRZEPLYWOWYCH IM ROBERTA SZEWALSKIEGO POLSKIEJ AKADEMII NAUK - IMP PAN
Organization address
address: UL. FISZERA 14 contact info |
| Nazionalità Coordinatore | Poland [PL] |
| Totale costo | 5˙096˙031 € |
| EC contributo | 3˙567˙790 € |
| Programma | FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics) |
| Code Call | FP7-AAT-2010-RTD-1 |
| Funding Scheme | CP-FP |
| Anno di inizio | 2012 |
| Periodo (anno-mese-giorno) | 2012-02-01 - 2016-01-31 |
Partecipanti
| # | ||||
|---|---|---|---|---|
| 1 |
INSTYTUT MASZYN PRZEPLYWOWYCH IM ROBERTA SZEWALSKIEGO POLSKIEJ AKADEMII NAUK - IMP PAN
Organization address
address: UL. FISZERA 14 contact info |
PL (GDANSK) | coordinator | 256˙928.00 |
| 2 |
DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV
Organization address
address: Linder Hoehe contact info |
DE (KOELN) | participant | 703˙900.00 |
| 3 |
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
Organization address
address: Avenue de la Division Leclerc 29 contact info |
FR (CHATILLON) | participant | 422˙750.00 |
| 4 |
NUMERICAL MECHANICS APPLICATIONS INTERNATIONAL SA
Organization address
address: CHAUSSEE DE LA HULPE 187-189 contact info |
BE (BRUXELLES) | participant | 270˙000.00 |
| 5 |
SA KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS OF SIBERIAN BRANCH OF RUSSIAN ACADEMY OFSCIENCE*ITAM OF SB RAS
Organization address
address: INSTITUTSKAYA 4/1 contact info |
RU (NOVOSIBIRSK) | participant | 232˙900.00 |
| 6 |
UNIVERSITA DEGLI STUDI DI ROMA LA SAPIENZA
Organization address
address: Piazzale Aldo Moro 5 contact info |
IT (ROMA) | participant | 232˙500.00 |
| 7 |
INSTYTUT LOTNICTWA
Organization address
address: KRAKOWSKA 110/114 contact info |
PL (WARSZAWA) | participant | 205˙850.00 |
| 8 |
TECHNISCHE UNIVERSITEIT DELFT
Organization address
address: Stevinweg 1 contact info |
NL (DELFT) | participant | 204˙300.00 |
| 9 |
INSTITUT NATIONAL POLYTECHNIQUE DE TOULOUSE
Organization address
address: ALLEE EMILE MONSO 6 contact info |
FR (TOULOUSE CEDEX 4) | participant | 161˙300.00 |
| 10 |
CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE
Organization address
address: Rue Michel -Ange 3 contact info |
FR (PARIS) | participant | 157˙775.00 |
| 11 |
THE CHANCELLOR, MASTERS AND SCHOLARS OF THE UNIVERSITY OF CAMBRIDGE
Organization address
address: The Old Schools, Trinity Lane contact info |
UK (CAMBRIDGE) | participant | 152˙800.00 |
| 12 |
UNIVERSITY OF SOUTHAMPTON
Organization address
address: Highfield contact info |
UK (SOUTHAMPTON) | participant | 148˙900.00 |
| 13 |
THE UNIVERSITY OF LIVERPOOL
Organization address
address: Brownlow Hill, Foundation Building 765 contact info |
UK (LIVERPOOL) | participant | 124˙187.00 |
| 14 |
DASSAULT AVIATION SA
Organization address
address: Rond-Point des Champs-Elysees - Marcel Dassault 9 contact info |
FR (PARIS) | participant | 118˙200.00 |
| 15 |
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
Organization address
address: Eschenweg 11 contact info |
DE (BLANKENFELDE-MAHLOW) | participant | 97˙000.00 |
| 16 |
THE PODGORNY INSTITUTE FOR MECHANICAL ENGINEERING PROBLEMS OF NATIONAL ACADEMY OF SCIENCE OF UKRAINE
Organization address
address: POZHARSKY STR 2/10 contact info |
UA (KHARKIV) | participant | 78˙500.00 |
Mappa
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Obiettivo del progetto (Objective)
'Vision-2020, whose objectives include the reduction of emissions and a more effective transport systems, puts severe demands on aircraft velocity and weight. These require an increased load on wings and aero-engine components. The greening of air transport systems means a reduction of drag and losses, which can be obtained by keeping laminar boundary layers on external and internal airplane parts. Increased loads make supersonic flow velocities more prevalent and are inherently connected to the appearance of shock waves, which in turn may interact with a laminar boundary layer. Such an interaction can quickly cause flow separation, which is highly detrimental to aircraft performance, and poses a threat to safety. In order to diminish the shock induced separation, the boundary layer at the point of interaction should be turbulent. The main objective of the TFAST project is to study the effect of transition location on the structure of interaction. The main question is how close the induced transition may be to the shock wave while still maintaining a typical turbulent character of interaction. The main study cases - shock waves on wings/profiles, turbine and compressor blades and supersonic intake flows - will help to answer open questions posed by the aeronautics industry and to tackle more complex applications. In addition to basic flow configurations, transition control methods (stream-wise vortex generators and electro-hydrodynamic actuators) will be investigated for controlling transition location, interaction induced separation and inherent flow unsteadiness. TFAST for the first time will provide a characterization and selection of appropriate flow control methods for transition induction as well as physical models of these devices. Emphasis will be placed on closely coupled experiments and numerical investigations to overcome weaknesses in both approaches.'