Impulsive start of a symmetric airfoil at high angle of attack

AIAA Journal

Volumn 34, Issue 2, 1996, Pages 225-230

  Katz, Joseph ^a,c   Yon, Steven ^a,c   Rogers, Stuart E ^b,c  

^a AGC Paul S Roel Chair in Construction Engineering and Management   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AEROFOILS; FLUID DYNAMICS; NAVIER-STOKES EQUATIONS; VORTEX SHEDDING;

COMPUTATIONAL METHODS; CONVERGENCE OF NUMERICAL METHODS; DYNAMIC RESPONSE; FLUID DYNAMICS; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; VORTEX FLOW; VORTEX SHEDDING;

ALTERNATING PERIODIC VORTEX SHEDDING; HIGH ANGLE OF ATTACK; IMPULSIVE START; SYMMETRIC AIRFOIL;

AIRFOILS;

EID: 0030072005     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.13054     Document Type: Article

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