First measurements on an Airbus high lift configuration at ETW up to flight Reynolds number

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Quest, Juergen ^a   Wright, Martin C ^a   Hansen, Heinz ^b   Mesuro, Gabriel G ^c  

^a ETW GmbH   (Germany)

^b AIRBUS OPERATIONS GMBH   (Germany)

^c AIRBUS GROUP INNOVATIONS   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

CODES (SYMBOLS); MACH NUMBER; SUPERSONIC AIRCRAFT; WIND TUNNELS;

AEROELASTIC EFFECTS; CRYOGENIC TEMPERATURES; EUROPEAN RESEARCH PROJECT; EXPERIMENTAL INVESTIGATIONS; FLIGHT REYNOLDS NUMBERS; LOW MACH NUMBERS; MODELING FEATURES; REYNOLDS NUMBER EFFECT;

REYNOLDS NUMBER;

EID: 85087599812     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-423     Document Type: Conference Paper

References (3)

1. Martin C.N. Wright Development of the Half Model Testing Capability at ETW ICAS 2000
2. Quest, J. ETW-High Quality Test Performance in cryogenic environment AIAA-00-2206
3. Schimanski, D. & Hefer, G. Recent Aspects of high Reynolds Number Data Quality and Capabilities at the European Transonic Windtunnel AIAA-00-0292