DR2 Aerodynamic PDR Aerodynamic Preliminary Design Review October 3, 2000 German National Holiday Presented By: Loren Garrison Team DR2 Chris Curtis Chris.

Slides:

Advertisements

Similar presentations

February 17, Aerodynamics 2 PDR Michael Caldwell Jeff Haddin Asif Hossain James Kobyra John McKinnis Kathleen Mondino Andrew Rodenbeck Jason Tang.

Advertisements

Ashley Brawner Neelam Datta Xing Huang Jesse Jones

SAE Aero Design ® East 2005 University of Cincinnati AeroCats Team #039 SAE Aero Design ® East 2005 University of Cincinnati AeroCats Team #039 Design.

AAE 451 Aircraft Design Aerodynamic Preliminary Design Review #2 Team Members Oneeb Bhutta, Matthew Basiletti, Ryan Beech, Mike Van Meter.

Presented by Dan Shafer James Pembridge Mike Reilly

DR2 Aerodynamic PDR II Aerodynamic Preliminary Design Review II “The 20 Hour Marathon” October 19, 2000 Presented By: Loren Garrison Team DR2 Chris Curtis.

Chase Beatty (Team Leader) Brian Martinez (Organizer) Mohammed Ramadan (Financial Officer) Noe Caro (Historian) SAE AERO Chase Beatty.

Lift and Drag Review and Renew

Aerodynamic Shape Optimization in the Conceptual and Preliminary Design Stages Arron Melvin Adviser: Luigi Martinelli Princeton University FAA/NASA Joint.

Keith Hout Patrick Dempsey Bridget Fitzpatrick Heather Garber Jong Soo Mok Stability Control and Flight Performance PDR October 24, 2000.

Project Presentation Boiler Xpress December 5, 2000 Team Members Oneeb Bhutta Matthew Basiletti Ryan Beech Micheal Van Meter AAE 451 Aircraft Design.

AAE 451 Aircraft Design Aerodynamic Preliminary Design Review #1

AME 441: Conceptual Design Presentation

DR2 Presented by: Mark Blanton Loren Garrison Chris Peters Jeff Rodrian September 26, 2000 Chris Curtis.

Dane BatemaBenoit Blier Drew Capps Patricia Roman Kyle Ryan Audrey Serra John TapeeCarlos Vergara Critical Design Review Team 1.

Aerodynamics PDR #1. Objective To examine airfoil choices To examine wing shape choices Structural and Manufacturing Concerns.

Click to edit Master title style Click to edit Master text styles Second level Third level Fourth level Fifth level 1.

DR2 Stability and Control Preliminary Design Review and Performance PDR October 24, 2000 Presented By: Christopher Peters …and that’s cool Team DR2 Chris.

Vehicle Sizing PDR Presented by: Mark Blanton Chris Curtis Loren Garrison September 21, 2000 Chris Peters Jeff Rodrian DR2.

Click to edit Master title style Click to edit Master text styles Second level Third level Fourth level Fifth level 1.

ME403 Chapter 3 Wing Aerodynamics

DR2 Propulsion PDR I Preliminary Design Review II October 17, 2000 Presented By: Mark Blanton Team DR2 Chris Curtis Loren Garrison Chris Peters Jeff Rodrian.

Patrick Dempsey Bridget Fitzpatrick Heather Garber Keith Hout Jong Soo Mok AAE451 Aircraft Design Professor Dominick Andrisani First Flight November 21,

Team 5 Aerodynamics QDR Presented By: Christian Naylor Charles Reyzer.

March 1, Aerodynamics 3 QDR Michael Caldwell Jeff Haddin Asif Hossain James Kobyra John McKinnis Kathleen Mondino Andrew Rodenbeck Jason Tang Joe.

Aero Engineering 315 Lesson 12 Airfoils Part I. First things first…  Recent attendance  GR#1 review  Pick up handout.

Aerodynamics QDR AAE451 – Team 3 October 9, 2003 Brian Chesko Brian Hronchek Ted Light Doug Mousseau Brent Robbins Emil Tchilian.

Team 5 Aerodynamics PDR Presented By: Christian Naylor Eamonn Needler Charles Reyzer.

DR2 Structures PDR Structures and Weight Preliminary Design Review October 5, 2000 Presented By: Jeff Rodrian & Chris Curtis Team DR2 Loren Garrison Chris.

Flight Performance, Stability and Control PDR Brian Barnett Rob Benner Ryan Srogi John Keune Alex Fleck.

Justin DeStories Aircraft Design. Objective/Requirements  The UAV team at Arizona State University is designing, optimizing, and building an autonomous.

SAE Aero Design ® East 2005 University of Cincinnati AeroCats Team #039 SAE Aero Design ® East 2005 University of Cincinnati AeroCats Team #039 Design.

AIAA Hybrid Airliner Competition 2013 The Transporters.

Team 5 Critical Design Review Trent Lobdell Ross May Maria Mullins Christian Naylor Eamonn Needler Charles Reyzer James Roesch Charles Stangle Nick White.

SAE AERO Chase Beatty (Team Leader) Brian Martinez (Organizer) Mohammed Ramadan (Financial Officer) Noe Caro (Historian) Chase Beatty.

Team “Canard” September 19th, 2006

Basic aerodynamics relationships

The Lumberjacks Team /16/12 Brian Martinez.

2D Airfoil Aerodynamics

1 Lecture 4: Aerodynamics Eric Loth For AE 440 A/C Lecture Sept 2009.

AAE 451 Aircraft Design First Flight Boiler Xpress November 21, 2000

Bridget Fitzpatrick Patrick Dempsey Heather Garber Keith Hout Jong Soo Mok Aerodynamics Preliminary Design Review #2 October 23, 2000.

AAE 451 AERODYNAMICS PDR 2 TEAM 4 Jared Hutter, Andrew Faust, Matt Bagg, Tony Bradford, Arun Padmanabhan, Gerald Lo, Kelvin Seah November 18, 2003.

Team 5 Aerodynamics QDR 2 Presented By: Christian Naylor Charles Reyzer.

February 24, Dynamics & Controls 1 PDR Michael Caldwell Jeff Haddin Asif Hossain James Kobyra John McKinnis Kathleen Mondino Andrew Rodenbeck Jason.

Airfoil Selection and Tail Design Jose Pedrego ASCEND Team 4/19/2008.

Airfoils. Airfoil Any surface that provides aerodynamic force through interaction with moving air Moving air Airfoil Aerodynamic force (lift)

Patrick Dempsey Bridget Fitzpatrick Heather Garber Keith Hout Jong Soo Mok Aerodynamics Preliminary Design Review #1 October 3, 2000.

DR2 Propulsion PDR I Preliminary Design Review September 28, 2000 Presented By: Mark Blanton Team DR2 Chris Curtis Loren Garrison Chris Peters Jeff Rodrian.

DR1 PF, E, & FTP PDR Prototype Fabrication, Economic and Flight Test Plan Preliminary Design Review October 26, 2000 Presented By: Mark Blanton & Chris.

AAE 451 AERODYNAMICS QDR 2 TEAM 4 Jared Hutter, Andrew Faust, Matt Bagg, Tony Bradford, Arun Padmanabhan, Gerald Lo, Kelvin Seah November 6, 2003.

Airfoil Any surface that provides aerodynamic force through interaction with moving air Aerodynamic force (lift) Moving air Airfoil.

Aerodynamics PDR AAE451 – Team 3 October 21, 2003

Dynamics & Controls PDR 1

Team 5 Final Design Review

Team 5 Final Design Review

Airfoils and Simulation

Cargo Airplane Challenge

Aether Aerospace AAE 451 September 27, 2006

Team “Canard” September 19th, 2006

UAV Wing Design For Efficiency At Low Reynolds Numbers

Team 5 Aerodynamics PDR #2

Aerodynamics PDR # 2 AAE451 – Team 3 November 18, 2003

Airfoils and Simulation

Team 5 Aerodynamics QDR #1

Airfoils and Simulation

Aether Aerospace AAE 451 September 19, 2006

Dynamic Modeling PDR Dynamic Modeling Preliminary Design Review for Vehicle and Avionics October 17, 2000 Presented By: Christopher Peters …and that’s.

Aether Aerospace AAE 451 September 6, 2006

Presentation transcript:

DR2 Aerodynamic PDR Aerodynamic Preliminary Design Review October 3, 2000 German National Holiday Presented By: Loren Garrison Team DR2 Chris Curtis Chris Peters Jeff Rodrian Mark Blanton

DR2 Aerodynamics PDR Airfoil Selection Procedure - Create an airfoil database - Based on experimental data from the NASG website - Reynolds Numbers of 100,000 and 150,000 - C l max of at least Refine Database - Based lift curves and drag polars - Selected three airfoils - Determine final airfoil - Based on lift curve, drag polar and endurance parameter

DR2 Aerodynamics PDR Lift Curves of Possible Airfoils

DR2 Aerodynamics PDR Drag Polars of Possible Airfoils

DR2 Aerodynamics PDR Lift Curves of Possible Airfoils

DR2 Aerodynamics PDR Drag Polars of Possible Airfoils

DR2 Aerodynamics PDR Endurance Parameters of Possible Airfoils

DR2 Aerodynamics PDR Wing Geometry - Airfoil:S Taper Ratio:0.7 - Dihedral Angle:0 (deg) - Sweep Angle:0 (deg) - Aspect Ratio:8 - Span:7.68 (ft) - Root Chord:1.13 (ft) - Tip Chord:0.79 (ft) - Planform Area:14.7 (ft 2 ) - Wetted Area:29.4 (ft 2 )

DR2 Aerodynamics PDR Horizontal Tail Geometry - Airfoil:Flat Plate - Taper Ratio: Dihedral Angle:0 (deg) - Sweep Angle:4.0 (deg) - Aspect Ratio:4 - Span:2.86 (ft) - Root Chord:0.82 (ft) - Tip Chord:0.61 (ft) - Planform Area:2.04 (ft 2 ) - Wetted Area:4.17 (ft 2 )

DR2 Aerodynamics PDR Vertical Tail Geometry - Airfoil:Flat Plate - Taper Ratio:0.6 - Dihedral Angle:0 (deg) - Sweep Angle:9.53 (deg) - Aspect Ratio:1.4 - Span:1.35 (ft) - Root Chord:1.29 (ft) - Tip Chord:0.72 (ft) - Planform Area:1.29 (ft 2 ) - Wetted Area:2.64 (ft 2 )

DR2 Aerodynamic PDR

DR2 Aerodynamics PDR 3-D Lift Curve

DR2 Aerodynamics PDR 3-D Lift Curve

DR2 Aerodynamics PDR 3-D Lift Curve

DR2 Aerodynamics PDR 3-D Lift Curve for the Aircraft

DR2 Aerodynamics PDR 3-D Drag Polar for the Aircraft

DR2 Aerodynamics PDR 3-D L/D Curve for the Aircraft

DR2 Aerodynamics PDR 3-D Endurance Parameter for the Aircraft