1 / 8

AEM 4331 Canard Design Meeting

AEM 4331 Canard Design Meeting. 10.05.2011. 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.

lavi
Download Presentation

AEM 4331 Canard Design Meeting

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. AEM 4331 Canard Design Meeting 10.05.2011

  2. 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

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

  4. 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

  5. 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

  6. 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

  7. 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

  8. Assignments for 10.07.11 • 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, Emails about Changes, Consolidation of current information

More Related