Wind tunnel test for flow control at the engine/pylon with a representative aircraft configuration under fully realistic flow conditions

Informacje na temat projektu

AFloWTest

Identyfikator umowy o grant: 738196

DOI 10.3030/738196

Projekt został zamknięty

Data podpisania przez KE 21 Grudnia 2016

Data rozpoczęcia 1 Stycznia 2017

Data zakończenia 31 Grudnia 2018

Finansowanie w ramach

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Koszt całkowity € 942 500,25

Wkład UE € 942 500,25

Koordynowany przez

STICHTING KONINKLIJK NEDERLANDS LUCHT - EN RUIMTEVAARTCENTRUM
Netherlands

Cel

The Active Flow Wind tunnel Test (AFloWTest) project considers the testing of a realistic high lift configuration half-model with a large and with a Ultra High Bypass Ratio (UHBR) flow-through nacelle. An existing half model will be adapted with an UHBR nacelle and for the application of Active Flow Control (AFC) systems at the upper side of the wing near the wing pylon interface in order to improve the high lift performance of the configuration. The application of AFC is considered in order to diminish the detrimental effects of applying a large nacelle in close proximity of the wing, necessitating a slat cutback. Different AFC systems will be installed and tested: a Pulsed Jet Actuator (PJA) and a Steady Blowing (SB) device. Each will be tested at one position. Low speed tests (Ma=0.1 to 0.3) need to be made at representatively high Reynolds number. With the target half model sufficiently high Reynolds number (Re based on mean aerodynamic chord) can only be obtained in a highly pressurized wind tunnel or in a cryogenic facility. The DNW-KKK cryogenic wind tunnel has been selected for the test.
Overall model forces will be measured and local influence of the AFC systems needs to be monitored, using surface streamline pattern visualization with mini-tufts, complemented with detailed PIV measurements of the separated flow and flow topology over the wing downstream of the wing pylon/nacelle interface.

Dziedzina nauki

• engineering and technology › electrical engineering, electronic engineering, information engineering › electronic engineering › sensors › optical sensors
• engineering and technology › mechanical engineering › vehicle engineering › aerospace engineering › aircraft
• natural sciences › physical sciences › classical mechanics › fluid mechanics › fluid dynamics
• engineering and technology › materials engineering
• engineering and technology › environmental engineering › energy and fuels

Program(-y)

• H2020-EU.3.4. - SOCIETAL CHALLENGES - Smart, Green And Integrated Transport Main Programme
• H2020-EU.3.4.5.1. - IADP Large Passenger Aircraft

Temat(-y)

• JTI-CS2-2016-CFP03-LPA-01-17 - Windtunnel test for flow control at the engine/pylon with a representative aircraft configuration under fully realistic flow conditions

Zaproszenie do składania wniosków

H2020-CS2-CFP03-2016-01

System finansowania

CS2-RIA - Research and Innovation action

Koordynator

STICHTING KONINKLIJK NEDERLANDS LUCHT - EN RUIMTEVAARTCENTRUM

• Wkład UE netto: € 870 000,25
• Adres: ANTHONY FOKKERWEG 2 ; 1059 CM Amsterdam ; Niderlandy
• Region: West-Nederland › Noord-Holland › Groot-Amsterdam
• Rodzaj działalności: Research Organisations
• Koszt całkowity: € 870 000,25

Uczestnicy (1)

TECHNISCHE UNIVERSITEIT DELFT

Niderlandy

• Wkład UE netto: € 72 500,00
• Adres: STEVINWEG 1 ; 2628 CN Delft
• Region: West-Nederland › Zuid-Holland › Delft en Westland
• Rodzaj działalności: Higher or Secondary Education Establishments
• Koszt całkowity: € 72 500,00