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Volumn 2, Issue , 1999, Pages 1232-1253
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Development of a helicopter airframe flight-by-flight fatigue load spectrum
a a a a |
Author keywords
[No Author keywords available]
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Indexed keywords
AIRFRAMES;
CRACK INITIATION;
CRACK PROPAGATION;
EQUATIONS OF MOTION;
FATIGUE OF MATERIALS;
FINITE ELEMENT METHOD;
FOURIER TRANSFORMS;
MATHEMATICAL MODELS;
SPECTRUM ANALYSIS;
STRESS ANALYSIS;
FLIGHT-BY-FLIGHT FATIGUE LOAD SPECTRUM;
FOURIER COORDINATE TRANSFORMATION (FCT);
MILITARY HELICOPTERS;
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EID: 0032647028
PISSN: 07334249
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Article |
Times cited : (7)
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References (9)
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