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Volumn 3985, Issue , 2000, Pages 121-129
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Active and passive structural design concepts for improved empennage effectiveness of aircraft
a
a
DAIMLER AG
(Germany)
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Author keywords
[No Author keywords available]
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Indexed keywords
BUCKLING;
FIGHTER AIRCRAFT;
FINITE ELEMENT METHOD;
FLIGHT DYNAMICS;
FLUTTER (AERODYNAMICS);
FUSELAGES;
MANEUVERABILITY;
OPTIMIZATION;
STABILITY CRITERIA;
STIFFNESS;
WEIGHT CONTROL;
ACTIVE STRUCTURE;
BUCKLING STABILITY;
FLUTTER STABILITY CRITERIA;
YAW EFFECTIVENESS;
EMPENNAGES;
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EID: 0033690252
PISSN: 0277786X
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1117/12.388816 Document Type: Conference Paper |
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Times cited : (4)
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References (9)
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