Three-dimensional unsteady flow computations around a conventional slat of high-lift devices

AIAA Journal

Volumn 46, Issue 5, 2008, Pages 1045-1053

  Imamura, Taro ^a,b,c   Enomoto, Shunji ^a,b,c   Yokokawa, Yuzuru ^a,b,c   Yamamoto, Kazuomi ^a,b,c  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Aviation Program Group   (Japan)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

(1 1 0) SURFACE; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS (AIAA); BROAD BAND NOISE; COMPUTATIONAL COSTS; COMPUTATIONAL DATA; COMPUTATIONAL RESULTS; DIFFERENT TYPES; GRID RESOLUTIONS; HIGH LIFT CONFIGURATION; HIGH LIFT DEVICES; HIGH-FREQUENCY (HF); HYBRID METHODS; IMPLICIT TIME INTEGRATION; LOW FREQUENCY (LF); NARROW BANDS; NAVIER STOKES; NUMERICAL SCHEMES; POWER SPECTRAL; PRESSURE COEFFICIENTS; REYNOLDS (CO); SLAT NOISE; SUBITERATIONS; THREE DIMENSIONAL (3D); UNSTEADY FLOW COMPUTATIONS; VORTICAL STRUCTURES;

AERODYNAMICS; AVIATION; COMPUTATIONAL METHODS; DATA STRUCTURES; EXPERIMENTS; FLUID DYNAMICS; FLUID MECHANICS; NUMBER THEORY; NUMERICAL METHODS; REYNOLDS NUMBER; THREE DIMENSIONAL; UNSTEADY FLOW; VORTICITY;

COMPUTATIONAL GEOMETRY;

EID: 44849094526     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.25660     Document Type: Conference Paper

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