Guidelines for computing longitudinal dynamic stability characteristics of a subsonic transport

28th AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2010, Pages

  Thompson, Joseph R ^a,b   Frink, Neal T ^b,c   Murphy, Patrick C ^b,c  

^a UNIVERSITY OF ALABAMA AT BIRMINGHAM   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Research Director   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

TRANSPORT AIRCRAFT; WIND TUNNELS;

COMPUTATIONAL SIMULATION; COMPUTATIONAL SOLUTIONS; FORCED OSCILLATIONS; LONGITUDINAL DYNAMICS; MOMENT COEFFICIENT; NUMERICAL PARAMETERS; NUMERICAL SOLUTION STRATEGIES; STABILITY DERIVATIVES;

FIGHTER AIRCRAFT;

EID: 78649505631     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2010-4819     Document Type: Conference Paper

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