Recent enhancements to USM3D unstructured flow solver for unsteady flows

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 2, Issue , 2004, Pages 925-937

  Pandya, Mohagna J ^a   Frink, Neal T ^b,d   Abdol Hamid, Khaled S ^b,d   Chung, James J ^c  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c NAVAL AIR SYSTEMS COMMAND   (United States)

^d Mail Stop 499 ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFOILS; FREQUENCIES; KINETIC ENERGY; PLASMA OSCILLATIONS; PRESSURE EFFECTS; REYNOLDS NUMBER; SHOCK TUBES; TURBULENT FLOW; UNSTEADY FLOW;

LIFT COEFFICIENT; MACH NUMBER; PRESSURE COEFFICIENTS; UNSTRUCTURED FLOW;

COMPUTATIONAL FLUID DYNAMICS;

EID: 20544434890     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-5201     Document Type: Conference Paper

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