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Volumn , Issue , 2008, Pages
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Application of an integrated approach to the UAV conceptual design
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Author keywords
[No Author keywords available]
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Indexed keywords
AIRCRAFT DESIGN PROCESS;
AIRCRAFT GEOMETRIES;
BLENDED WING BODY;
CERTIFICATION REQUIREMENTS;
COMPREHENSIVE ANALYSIS;
COST SAVING;
DESIGN PROBLEMS;
DESIGN PROCESS;
DESIGN PROGRESS;
DESIGN QUALITY;
FLYING WINGS;
INTEGRATED APPROACH;
MANUFACTURABILITY;
MS EXCEL;
PRECISION FARMING;
RECTANGULAR WINGS;
AERODYNAMIC STABILITY;
AERODYNAMICS;
AGRICULTURE;
AIRCRAFT;
COMPUTATIONAL FLUID DYNAMICS;
COMPUTATIONAL GEOMETRY;
COMPUTER AIDED DESIGN;
CONCEPTUAL DESIGN;
COST BENEFIT ANALYSIS;
ENVIRONMENTAL REGULATIONS;
INTEGRATED CONTROL;
MANUFACTURE;
PRODUCT DESIGN;
STRESS INTENSITY FACTORS;
STRUCTURAL ANALYSIS;
AVAILABILITY;
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EID: 78149446231
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (14)
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References (14)
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