Multidisciplinary issues in airframe design

37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference

Volumn , Issue , 1996, Pages 609-619

  Venkayya, V B ^a   Tischler, V A ^a   Bharatram, G ^b  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b WRIGHT STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN; STRUCTURAL DYNAMICS; AERODYNAMIC LOADS; ALGORITHMS; COMPUTER SIMULATION; COMPUTER SOFTWARE; DYNAMIC RESPONSE; FINITE ELEMENT METHOD; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; OPTIMIZATION; SYSTEMS ANALYSIS; WINGS;

AIRFRAME DESIGN; ANTI-SYMMETRIC; DESIGN STUDIES; MINIMUM WEIGHT; MULTI-DISCIPLINARY OPTIMIZATIONS; OPTIMAL DESIGN; WING DESIGN; WING SWEEP;

STRUCTURAL DESIGN; AIRFRAMES;

AIRCRAFT RESPONSE; MULTIDISCIPLINARY OPTIMIZATION SYSTEM; STATIC AIRLOADS; WING SWEEP;

EID: 0029718375     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1386     Document Type: Conference Paper

References (13)

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