Six degree of freedom computation of the F-15E entering a spin

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 14, Issue , 2006, Pages 10234-10242

  Forsythe, James R ^a,b,d   Strang, William Z ^a   Squires, Kyle D ^c,d  

^a Cobalt Solutions LLC ^*  (United States)

^b AIR FORCE OFFICE OF SCIENTIFIC RESEARCH   (United States)

^c ARIZONA STATE UNIVERSITY   (United States)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; COMPUTATIONAL METHODS; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); FLOW FIELDS; SPIN DYNAMICS;

ASYMMETRIC VORTEX; DETACHED EDDY SIMULATION (DES); HORIZONTAL ATTITUDE; YAWING MOMENT;

AEROSPACE VEHICLES;

EID: 34250727567     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-858     Document Type: Conference Paper

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