ICTACEM 2025
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Validating Combined Vector Field Approach with
Full Quadrotor Dynamics
Aircraft Design and Optimization Lab
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WEEK 1- Business Jet Survey
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WEEK 2- Conceptual Design of Business
Class Jet
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WEEK 3- Comprehensive Wing Design
Analysis
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WEEK 4- Initial Estimation of Thrust to
Weight Ratio (T/W) and Wing Loading (W/S) of a
Business Jet
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WEEK 5- Initial Sizing of a Business
Jet
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WEEK 6- CAD Design and
Specifications
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WEEK 7
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Internal Configuration, Landing Gear,
and Aerodynamic Performance Validation
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Weight Estimation, Load Validation, and
Structural Configuration
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WEEK 8- Static Stability Analysis
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WEEK 9- Full Combined Presentation