Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 1, Issue , 1998, Pages 87-98

  Rouse, Marshall ^a   Ambur, Damodar R ^a   Dopker, Bernard ^a   Shah, Bharat ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FUSELAGES; PRESSURE EFFECTS; SANDWICH STRUCTURES; STRUCTURAL ANALYSIS; STRUCTURAL PANELS; TENSILE TESTING; TRANSPORT AIRCRAFT;

BIAXIAL TENSION LOADING; DESIGN LOAD LIMIT;

COMPOSITE STRUCTURES;

EID: 0031652904     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)