Adjoint-based adaptive mesh refinement for sonic boom prediction

Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn , Issue , 2008, Pages

  Wintzer, Mathias ^a,d   Nemec, Marian ^b,d,e   Aftosmis, Michael J ^c,d,e  

^a STANFORD UNIVERSITY   (United States)

^b ELORET CORPORATION   (United States)

^c NASA AMES RESEARCH CENTER   (United States)

^d Department of Aeronautics and Astronautics ^*

^e MS T27B

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ASPECT RATIO; FIGHTER AIRCRAFT; SHOCK WAVES;

ADAPTIVE MESH REFINEMENT; AXISYMMETRIC BODIES; DISCRETIZATION ERRORS; PROPAGATED SIGNALS; SHAPED SONIC BOOM DEMONSTRATIONS; SURFACE GEOMETRIES; THREE DIMENSIONAL GEOMETRY; WING-BODY CONFIGURATIONS;

MESH GENERATION;

EID: 85067320777     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-6593     Document Type: Conference Paper

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