Unsteady low mach preconditioning with application to rotorcraft flows

Collection of Technical Papers - 18th AIAA Computational Fluid Dynamics Conference

Volumn 2, Issue , 2007, Pages 1941-1961

  Potsdam, Mark A ^a,d,e   Sankaran, Venkateswaran ^b,e,f   Pandya, Shishir A ^c,e,g  

^a US Army AMRDEC Development   (United States)

^b UNIVERSITY OF CALIFORNIA   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

^d M S 215 1   (United States)

^e AIAA   (United States)

^f MS 215 1   (United States)

^g MS T27B 1   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; CONVERGENCE OF NUMERICAL METHODS; MACH NUMBER; NAVIER STOKES EQUATIONS; ROTORS; VORTEX FLOW;

ARTIFICIAL DISSIPATION MODEL; FUSELAGE CONFIGURATION; HELICOPTER ROTOR; ROTORCRAFT FLOWS;

UNSTEADY FLOW;

EID: 35648943634     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-4473     Document Type: Conference Paper

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