Numerical investigation of slat and compressibility effects for a high-lift wing

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Baker, M David ^a,c   Matbias, Donovan L ^a,c   Roth, Karlin R ^a   Cummings, Russell M ^b,d  

^a NASA AMES RESEARCH CENTER   (United States)

^b CALIFORNIA POLYTECHNIC STATE UNIVERSITY   (United States)

^c Integrated Systems Technologies Branch   (United States)

^d Integrated Systems Technology Branch ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; ANGLE OF ATTACK; COMPRESSIBILITY; FLOW SEPARATION; INCOMPRESSIBLE FLOW; KNOWLEDGE BASED SYSTEMS; NASA; NUMERICAL MODELS; REYNOLDS NUMBER; WIND TUNNELS;

CHORD-BASED REYNOLDS NUMBER; COMPRESSIBILITY EFFECTS; COMPRESSIBLE NAVIER-STOKES EQUATIONS; GLOBAL EFFECTS; LANDING CONFIGURATIONS; MODELING TECHNIQUE; NUMERICAL INVESTIGATIONS; SURFACE PRESSURE MEASUREMENTS;

NAVIER STOKES EQUATIONS;

EID: 84983212549     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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