Experimental investigation of a simplified 3D high lift configuration in support of CFD validation

18th Applied Aerodynamics Conference

Volumn , Issue , 2000, Pages

  Johnson, Paul L ^a   Jones, Kenneth M ^b   Madson, Michael D ^c  

^a BOEING COMPANY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CODES (SYMBOLS); COMPUTATIONAL FLUID DYNAMICS; NASA; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; WIND TUNNELS; WINGS;

CURRENT GENERATION; EXPERIMENTAL INVESTIGATIONS; HIGH LIFT SYSTEM; LANDING CONFIGURATIONS; NAVIER-STOKES CODE; PRESSURE PROBES; TRANSITION LOCATIONS; VELOCITY PROFILES;

LIFT;

EID: 85086614184     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4217     Document Type: Conference Paper

References (20)

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