MAE 155B - Aerospace Engineering Design II

Unmanned Aerial Vehicle

Spring Quarter - Mondays and Wednesdays 5:00pm - 6:50pm WLH 2113

Textbook

Aircraft Design: A Conceptual Approach
Daniel P. Raymer, AIAA Education Series, Fourth Edition (2006)



Lectures

• Lecture 0
• Lecture 1 - Overview
• Lecture 2 - Requirements Development
• Lecture 3 - Sizing; Design Reviews & Reports
• Lecture 4 - Configuration & Layout; Aerodynamics
• Lecture 5 - Structures, Loads, and Mass Properties
• Lecture 6 - Performance Analysis & Estimation
• Lecture 7 - Subsystems & Payload Integration, Part 1
• Lecture 8 - Subsystems & Payload Integration, Part 2
• Lecture 9 - Stability & Control, Handling Qualities
• Lecture 10 - Drag Polar Development
• Lecture 11 - Flight Testing, presented by M.L. Martin
• Lecture 12 - Final Proposal Structure
• Lecture 13 - Cost, MDO, Certification
  
  

  Pegasus Proposal (2007)

• Presentation 1 - Aircraft Requirements
• Presentation 2 - SRR
• Presentation 3 - Risk Reduction Project and Airfoil Selection
• Presentation 4 - Testing, MDD, and Tail Placement
• Presentation 5 - Risk Reduction Results, BFL, Weight Buildup, Wing and Airfoil Design
• Proposal Presentation - Final proposal presentation
• Proposal Report - Final proposal report
  
  

  Design Input Files

• Engine Deck: (Excel 2000) (Excel 1997)
• Atmosphere Model: airprop.mat, based on Table B.1-1 in Aircraft Design: A Conceptual Approach
• AVL Example File: AVL