PROPULSION PDR 1 AAE 451 TEAM 4

Slides:

Advertisements

Similar presentations

6.6 Interaction between a hull & a propeller

Advertisements

Heat Exchanger Design Thermal / Fluid System Design Final Project Department of Mechanical Engineering Fall 2005 December 13, 2005 Team Members: Andrew.

Evaluating Propeller Cuts Using Photographs of Marine Mammal Carcasses and Living Animals James L. Wood Lumatrex, Inc. Evaluating Propeller.

Airplane Flight: X-Plane in the Classroom Power Loading Ratio of the plane’s weight divided by power.

Lab 07: System Analysis 3 (Wind Tunnel Testing) Advanced Energy Vehicle.

Lab 06: AEV System Analysis 2 Advanced Energy Vehicle (AEV)

Propulsion PDR 1 Team 1 September 21, 2006.

SAE Aero Design Guidelines Rev A, 2013 Aero Design Oral Presentation Guidelines How to Deliver a Presentation The Judges will Notice.

Modular Carbon Fiber Propeller Kevin Cullen, Thomas Cummings, Rob Edsall, Sam Henry Undergraduate, Marine Engineering Technology Methods Design Create.

1 Design Group 2 Kat Donovan - Team Leader Andrew DeBerry Mike Kinder John Mack Jeff Newcamp Andrew Prisbell Nick Schumacher Conceptual Design for AME.

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

Propulsion QDR 2 AAE 451 Fall 2006 Team 4 Tung TranMark Koch Matt Drodofsky Matt Lossmann Ravi PatelKi-bom Kim Haris Md IshakAndrew Martin.

AAE 450 – Spacecraft Design 1 Mars Entry Aerodynamic Design Mark W. Vahle 18 January 2005 Aerodynamics Team Also working with Propulsion, Thermal, and.

October 23, 2003Propulsion QDR1 Scott Bird Mike Downes Kelby Haase Grant Hile Cyrus Sigari Sarah Umberger Jen Watson.

Propulsion QDR #2 AAE451 – Team 3 November 20, 2003 Brian Chesko Brian Hronchek Ted Light Doug Mousseau Brent Robbins Emil Tchilian.

March 8, Propulsion 3 QDR Michael Caldwell Jeff Haddin Asif Hossain James Kobyra John McKinnis Kathleen Mondino Andrew Rodenbeck Jason Tang Joe Taylor.

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.

Propulsion PDR #2 Brian Barnett Rob Benner Ryan Srogi John Keune Alex Fleck.

1 Propulsion PDR Ashley Brawner Matt Negilski Neelam Datta Mike Palumbo Xing Huang Chris Selby Jesse Jones Tara Trafton AAE451: Balsa to the Wall Team.

Dane BatemaBenoit Blier Drew Capps Patricia Roman Kyle Ryan Audrey Serra John TapeeCarlos Vergara Team 1: Propulsion QDR 2 Team 1 October 3, 2006.

Propulsion PDR 2 Team Boiler Xpress Michael VanMeter Oneeb Bhutta Matthew Basiletti Ryan Beech October 17, 2000.

Aero Design Group 10 Dimitrios Arnaoutis Alessandro Cuomo

Lab 06: AEV System Analysis 2 Advanced Energy Vehicle (AEV)

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

1 Conceptual Design Review 4/17/07 Team 1 John Horst John Horst Jared Odle Jared Odle Keith Fay Keith Fay Boyce Dauby Boyce Dauby Andrew Kovach Andrew.

Propulsion PDR #2 AAE451 – Team 3 November 11, 2003 Brian Chesko Brian Hronchek Ted Light Doug Mousseau Brent Robbins Emil Tchilian.

Patrick Dempsey Bridget Fitzpatrick Heather Garber Keith Hout Jong Soo Mok Propulsion Preliminary Design Review #2 October 17, 2000.

Miguel Jimenez Ricardo Lugo Carlos Rojas Advisor: Andres Tremante.

Project Plan Review Boiler Xpress Oneeb Bhutta Ryan Beech Matt Basiletti Mike VanMeter.

First-Year Engineering Program Advanced Energy Vehicle System Analysis 3 Reference:  AEV Lab Manual  System Analysis 3 Grading Guidelines.

Team 5 Vehicle Propulsion QDR 2 Presented By: Maria Mullins James Roesch.

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

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

Dane BatemaBenoit Blier Drew Capps Patricia Roman Kyle Ryan Audrey Serra John TapeeCarlos Vergara Team 1: Propulsion QDR 3 Team 1 October 17, 2006.

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

Solar Cup Boat Design Information for rookies

STRUCTURES & WEIGHTS PDR 1

VEHICLE SIZING PDR AAE 451 TEAM 4

Propulsion PDR 1 Team #3 Presented by: Greg Davidson Etan Karni

DYNAMICS & CONTROL PDR 1 TEAM 4

The Aircraft Engine Design Project- Engine Cycles

Propulsion QDR 2 Team #3 Presented by: Greg Davidson Etan Karni.

Team 5 Final Design Review

PROPULSION PDR 2 AAE 451 TEAM 4

Team 5 Propulsion PDR Scott Bird Mike Downes Kelby Haase Grant Hile

CRITICAL DESIGN REVIEW

STRUCTURES & WEIGHTS PDR 2

Team 5 Final Design Review

Aether Aerospace AAE 451 October 3, 2006

Propulsion 2 QDR AAE 451: Team 2 Michael Caldwell Jeff Haddin

Solo-1 ARF Airplane Team 4: Joshua Shawala (Team Leader) Darth Fitch

Propulsion PDR AAE 451 Fall 2006 Team Whishy Washy Tung Tran Mark Koch

Team 5 Vehicle Propulsion PDR 1

Team 5 Vehicle Propulsion PDR 1

John Apostol, Chris Grupido, Douglas Klutzke

Propulsion PDR AAE 451: Team 2 Michael Caldwell Jeff Haddin

Team 5 – Propulsion QDR #2 Scott Bird Mike Downes Kelby Haase

DYNAMICS & CONTROL QDR 1 TEAM 4

COST QDR TEAM 4 Jared Hutter, Andrew Faust, Matt Bagg, Tony Bradford,

Aether Aerospace AAE 451 September 19, 2006

DYNAMICS & CONTROL QDR 3 TEAM 4

PROPULSION QDR 1 AAE 451 TEAM 4

Team 5 - Propulsion PDR #2 Scott Bird Mike Downes Kelby Haase

Propulsion QDR Scott Bird Mike Downes Kelby Haase Grant Hile

PROPULSION QDR 2 AAE 451 TEAM 4

Propulsion PDR #1 AAE451 – Team 3 October 7, 2003

STRUCTURES & WEIGHTS QDR 1

Team 5 Vehicle Sizing PDR

Vehicle Sizing PDR AAE451: Balsa to the Wall

Propulsion QDR AAE 451 Fall 2006 Team 4 Tung Tran Mark Koch

Presentation transcript:

PROPULSION PDR 1 AAE 451 TEAM 4 Jared Hutter, Andrew Faust, Matt Bagg, Tony Bradford, Arun Padmanabhan, Gerald Lo, Kelvin Seah October 7, 2003

OVERVIEW Preliminary Engine Selection Propeller Analysis Conclusions Follow-Up Actions

PRELIMINARY ENGINE SELECTION From the Constraint Analysis, Power Loading, W/P = 22.42 lbf / SHP From Preliminary Weight Estimate, Gross Take-Off Weight, WTO = 54.52 lbf Total Required Power = 2.45 HP Twin Engine Considerations

PRELIMINARY ENGINE SELECTION Source: http://www.globalhobby.com/magnum/magxl.htm

PRELIMINARY ENGINE SELECTION Engine Choice: Magnum XL 75 Specifications: Bore: 26.8 mm Stroke: 22.0 mm Practical RPM: 2,000 - 12,000 Power: 2.30 BHP Weight 21.7 oz

PROPELLER ANALYSIS Fixed pitch to be 7” based on recommendation for the selected engine. Varied propeller diameter between 10” and 14”. Varied RPM between 5,000 and 13,000 rev/min. Plotted CP, CT, HP and ηp versus J. Varied pitch and re-analyzed the data. Design point selected.

PROPELLER ANALYSIS Decreasing RPM

PROPELLER ANALYSIS Decreasing RPM

PROPELLER ANALYSIS

PROPELLER ANALYSIS CLOSE UP 8000 RPM

PROPELLER ANALYSIS ηp = 0.545

PROPELLER ANALYSIS CLOSE UP ηp = 0.545

PROPELLER ANALYSIS for Dia = 13” Design Point Decreasing Diameter

PARAMETERS PRELIMINARY Diameter: 13” Pitch: 7” RPM: 8,000 rev/min Power: 1.24 HP Advance Ratio: 0.3165 rev-1 Power Coefficient: 0.0358 Thrust Coefficient: 0.0616 Efficiency: 54.5% 13” x 7” $29

FOLLOW-UP ACTIONS Analysis for twin-engine operation. Analysis for engine-out condition.

QUESTIONS?