Development of a new potential flow based model for hover performance prediction

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 5361-5379

  Bhagwat, Mahendra ^a,c,d   Moulton, Marvin A ^b,d,e   Caradonna, Francis X ^b,c,d  

^a ELORET CORPORATION   (United States)

^b US Army AMRDEC Development   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

^d AIAA   (United States)

^e Aeromechanics Division

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; COMPUTATIONAL FLUID DYNAMICS; CONVERGENCE OF NUMERICAL METHODS; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; VORTEX FLOW; WAKES;

FLOW FIELDS; HOVER PERFORMANCE; LAGRANGIAN CONVECTION; RAYNOLDS-AVERAGED NAVIER-STOKES (RANS) SOLVERS;

POTENTIAL FLOW;

EID: 30744433374     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-1367     Document Type: Conference Paper

References (12)

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