Numerical simulation of rolling-airframes using a multi-level cartesian method

20th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2002, Pages

  Murman, Scott M ^a   Aftosmis, Michael J ^b   Berger, Marsha J ^c  

^a ELORET CORPORATION   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c NEW YORK UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SURFACES; FLIGHT DYNAMICS; MISSILES; NUMERICAL METHODS; SUPERSONIC AIRCRAFT;

CARTESIAN METHOD; DYNAMIC COMPUTATIONS; DYNAMIC EFFECTS; MANEUVERABLE MISSILES; ROLLING MISSILE; STABILITY DERIVATIVES; TIME-DEPENDENT DYNAMICS; VISCOUS SIMULATIONS;

FLIGHT SIMULATORS;

EID: 85067321890     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-2798     Document Type: Conference Paper

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