Reduced-order models for a shallow curved beam under combined loading

AIAA Journal

Volumn 48, Issue 1, 2010, Pages 47-55

  Spottswood, S Michael ^a   Hollkamp, Joseph J ^a   Eason, Thomas G ^a  

^a AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC LOADING; AIRCRAFT STRUCTURE; COMBINED LOADING; COMMERCIAL FINITE ELEMENT CODES; CURVED BEAM STRUCTURES; CURVED BEAMS; CURVED STRUCTURE; DESIGN SPACES; ELEVATED TEMPERATURE; EXTREME ENVIRONMENT; GEOMETRIC NON-LINEAR; HYPERSONIC VELOCITY; PLANAR STRUCTURE; PRESSURE LOAD; REDUCED ORDER MODELS; REDUCED-ORDER MODELING; SONIC FATIGUE; STEALTHY AIRCRAFT; STOCHASTIC LOADING; THERMAL CONDITION; U.S. AIR FORCE; VARYING TEMPERATURE;

ACOUSTICS; AIRCRAFT ENGINES; AIRCRAFT MANUFACTURE; AIRFRAMES; CURVED BEAMS AND GIRDERS; HYPERSONIC VEHICLES; LOADS (FORCES);

STRUCTURAL DESIGN;

EID: 77049120349     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.38707     Document Type: Article

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