Objectives Pick one final design (Only discussions crucial to design choice will be allowed to occur) Note that many exact locations for many internal things will be decided with moment equations at a later time

Agenda Review from Cirrus Trip Ideas and Information for Design Update on Pull vs. Push Establish Design Choice Engine Location Tail Design Wing Design

Meeting Outcomes Design Scope Develop Minimal Top Design In-depth Analysis on Specific Aspects Pick Design to Proceed With Areas of Analysis for Aircraft Schedule for Proceeding

Design Scope Meeting With Cirrus Desire for stronger Trade Studies on Specific aspects of the aircraft Need for an overall design that still meets requirements Talk with Garrard about new direction of Project Decided on final concept design similar to the Velocity XL and the Cozy Mark IV with a two lifting surface configuration and a rear mounted engine

Areas of Interest for Analysis Landing Gear Design: Chris Erickson and Nathan Love Control Surface Analysis: Patrick Mischke Canard Configuration Analysis: Traci Moe Wing Design: Vince Zander General Body Analysis: Brian Douglas Lifting Surface Styles: Brad Lester Moment Analysis: Chris Schumacher

Schedule Analysis (Things done by date listed) Oct 10: PDR with Garrard 4:00 – 4:30 Oct 14: Initial Aircraft Design (Group Development) Oct 28: In Class PDR 3:35 – 4:05 Oct 31: Preliminary Individual Work Nov 21: Individual Analysis Completed Nov 28: Redesign of Preliminary Aircraft Dec 2: CDR Presentation Completed TBD: Final CDR

Assignments for Nate: Landing Gear estimates in weights and sizes Erickson: Landing Gear estimates in weights and sizes Traci: Canard Size and Weight, Fuselage Development Vince: Wing and Fuel Dimensions and Weights, Fuselage Development Brad: Equation Development for Requirements Brian: Equation Development for Requirements Schumacher: New Gantt Chart, New Schedule Development, s about Changes, Consolidation of current information