Blended Winglets on an E-Racer Canard Aircraft

Similar documents
Marc J. Zeitlin July 26 th, :30 PM 3:45 PM Forum Tent 06 Sporty s Pavilion. Rutan Derivative Canard Forum Slide #1

Marc J. Zeitlin July 31, :30 PM 3:45 PM Forum Tent 06 Utah Valley University Pavilion. Rutan Derivative Canard Forum Slide #1

COZY AIRCRAFT FORUM Soup to Nuts*?

How to use the Multirotor Motor Performance Data Charts

Friday, 27 June Realizing a small UAV for medical transport in developing countries Master thesis: Ferdinand Peters. Dr.One

... BY: Scott Barnhart

Building a Mick Reeves 1/4.5 scale Hurricane. Instalment 1

Welcome to the Airbus A380 Basic Manual for Virtual Air Cadet Airlines.

The low wing Cessna 170 a great idea that didn t fly

ECO-CARGO AIRCRAFT. ISSN: International Journal of Science, Engineering and Technology Research (IJSETR) Volume 1, Issue 2, August 2012

The Mark Ortiz Automotive

Santos-Dumont 15-bis. North American Valkyrie - NASA. The History of Canards

The scale model RC airplane: How to find the balance point (C.G.)

Design Considerations for Stability: Civil Aircraft

Full-Scale 1903 Wright Flyer Wind Tunnel Test Results From the NASA Ames Research Center

Model builder s Eye Boeing 787

Here is the gap seal I used for the flaps, genuine hardware store quality. Note cross sectional shape visible on the right end.

COMP AIR 10 Flagship of the Aerocomp Fleet Text by Norm Goyer Photos by Bill Fedorko

The following slideshow and talk were presented at the Uber Elevate Summit on April 25 th, The text included here is an approximate transcript

JR XP9303 Programming Guide for the Hangar Size P-51

Thank you again, Jim McCormick. Jabiru Pacific LLC

Mc Donnell Douglas F-4D Blk.37 Phantom II (J79-GE-15)

Prime Aircraft, LLC Aircraft Sales & Acquisitions

Sheffield Hallam University Engineering Masterclass Programme 2015

On-Demand Mobility Electric Propulsion Roadmap

Weight & Balance. Let s Wait & Balance. Chapter Sixteen. Page P1. Excessive Weight and Structural Damage. Center of Gravity

XIV.C. Flight Principles Engine Inoperative

Composite Modification Workshop AC Appendices

Terry Schubert - EZ.org/CSA. Flow Visualization Aids Drag Reduction

CHOOSING THE DESIGN OF YOUR AIRCRAFT

Caution Notes. Features. Specifications. Installation. A3 3-axis Gyro & Stabilizer User Manual V1.0

The BUGATTI 100P Replica Propeller(s) By Jan Carlsson January 2012

1 b. Definition and Discussion of the Intrinsic Efficiency of Winglets. Dieter Scholz. Hamburg University of Applied Sciences

AIRCRAFT DESIGN SUBSONIC JET TRANSPORT

CHAPTER 10. WEIGHT AND BALANCE

Building the HP-24 (Project) Bob Kuykendall 19 November 2005

Mc Donnell Douglas F-4E Blk.41 Phantom II (J79-GE-17)

Optimizing Plane Performance by Finding the Right Prop 10/15/09

Canards. Evan Neblett Mike Metheny Leifur Thor Leifsson. AOE 4124 Configuration Aerodynamics Virginia Tech 17. March 2003

Turbinator-2 Build Manual

The Ericksons highly modified Pacer BUDD DAVISSON

a Challenge for Lift-Based, Rigid Wing AWE Systems

FLIGHT TEST PROGRAM YOUR AIRPLANE HERE FLIGHT TEST PROGRAM YOUR AIRPLANE HERE

Supermarine Sparrow I 36 R/C Scale Model Instructions

ROBUST AIRFRAME FOR UAV FLIGHT TESTING FOR SALE!

Weight Effects Part 1

EASA TYPE-CERTIFICATE DATA SHEET EASA.A.038 SWIFT S-1

Blast Off!! Name. Partner. Bell

First test prop : Sensenich 54X54 wood prop

EXPERIMENTAL RESEARCH ON HELICOPTER TAIL SHAKE PHENOMENON

IAC AirVenture Plans and Information Celebrating One Design and Acro Sport Anniversaries. EAA AirVenture July 2017 Oshkosh, Wisconsin USA

Uncontrolled copy not subject to amendment. Airframes. Revision 1.00

Improving the gearshift feel in an SW20.

Preview of the Club Project Plane

Once again, another four weeks have gone by and I am quite sure everyone is tired of me wondering where the time has gone. To say that everything

January 2003 WELCOME SHOCKS WANTED FOR RESEARCH

Small Fixed Wing Aircraft Operational Weight and Balance Computations

Lip wing Lift at zero speed

The Magic of Electric Flying or. Volts and Amps for Dummies By John Wheater

Compared Air Combat Performances analysis Mig-21 versus F-5E

EASA TYPE-CERTIFICATE DATA SHEET EASA.A.574. SZD-54 Perkoz. Allstar PZL Glider Sp. z o.o.

The Next Meeting is Saturday June 18, 2016 at. 6:30 PM at the Hermon D. Lowery Field. Officers. AMA Chapter #755. June, 2016

Reducing Landing Distance

LAA TYPE ACCEPTANCE DATA SHEET TADS 064 STEEN SKYBOLT

Roehrig Engineering, Inc.

Powertrain Design for Hand- Launchable Long Endurance Unmanned Aerial Vehicles

Pipistrel ALPHA Trainer

DEVELOPMENT OF A CARGO AIRCRAFT, AN OVERVIEW OF THE PRELIMINARY AERODYNAMIC DESIGN PHASE

Insight. Hyperloop transportation of the future

AVOIDING THE BENDS! Why Super-Roc Models Buckle and How to Design for a Successful Flight. by Chris Flanigan (NAR L1)

ESPA3D Photo Essay One page ESPA3D Plans are HERE Back to Spad Plans Index

Turbo Dynamics Z1/F1100T ECU reflash with four switch positions

The winner team will have the opportunity to perform a wind tunnel test campaign in the transonic/supersonic Wind tunnel at the VKI.

MOTOR VEHICLE FUEL ECONOMY BY RICHARD STONE DOWNLOAD EBOOK : MOTOR VEHICLE FUEL ECONOMY BY RICHARD STONE PDF

The Sky Screamer makes it easy and affordable to develop

Normal T/O Procedure. * * * Engine Failure on T/O * * *

cutting down weight as much as possible and using available off-the-shelf light weight materials and RC equipment.

Electric VTOL Aircraft

THRUSTLINES Indianapolis R/C Modelers Chapter September 2017

Program Summary Model 281 Proteus

The Volt Vette Project

Chapter 10 Miscellaneous topics - 2 Lecture 39 Topics

Experiment 4 Topic: Solar Panel Week B Procedure

SIZING POWER SYSTEMS FOR ELECTRIC AIRPLANES

INDEX. Preflight Inspection Pages 2-4. Start Up.. Page 5. Take Off. Page 6. Approach to Landing. Pages 7-8. Emergency Procedures..

Primary control surface design for BWB aircraft

Cooling Systems For Automotive Conversion Part 4

THE NEW STEMME SKY CRUISER S12-SW.

DUCHESS BE-76 AND COMMERCIAL MULTI ADD-ON ORAL REVIEW FOR CHECKRIDE

2.11 Other Equipment and Installations

by John Glezellis 38 MODEL AVIATION

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A49NM

The implementation of highly advanced and efficient +25 kw RESLS - Retractable Electric Self-Launching System,

New Design Concept of Compound Helicopter

Ultralight airplane Design

SCHOOL OF COMPUTING, ENGINEERING AND MATHEMATICS SEMESTER 2 EXAMINATIONS 2013/2014 ME110. Aircraft and Automotive Systems

Part 1. The three levels to understanding how to achieve maximize traction.

Assembly and Operating Manual. SPECIFICATION Length inch (640mm) Wing Span inch (705mm) Flying Weight oz (330g)

Test of. Boeing MH-47G Chinook. Produced by Area-51 Simulations

Mid Hudson Radio Control Society. Pilot Briefing. Volume 6 Issue 11 November 2014

Transcription:

Blended Winglets on an E-Racer Canard Aircraft Performance Increase? Marc J. Zeitlin / Jack Morrison July 26 th, 2007 2:30 PM 3:45 PM Forum Tent 06 Sporty s Pavilion July 19, 2007 Canard Forum Slide Show Slide #1

What Will I Talk About? Introduction Who Am I? Who s Plane Is It? Consulting Process Aerodynamics of Canard Aircraft Winglets Modification Process Aircraft Configuration Before / After Aircraft Testing Aircraft Performance Before / After Performance Graphs Other Performance Differences? Extension to Other Canard Aircraft? Questions and Answers July 19, 2007 Canard Forum Slide Show Slide #2

Who The Heck Am I? Biography / Resume' http://www.mdzeitlin.com/marc/bio.html Loved planes since 3 years old - Built zillions of model aircraft Thesis - Design, Construction and Testing of an Electromagnetically Launched Model Glider Built Quickie Q2 Built COZY MKIV #386, N83MZ ~500 flying hours Started / Administer Unofficial COZY Builders Web Page and COZY Mailing List Work for Scaled Composites as Mechanical Engineer in charge of transitioning SS2/WK2 from prototype to production by The Spaceship Company Do Homebuilder Aircraft consulting for folks I like on the side July 19, 2007 Canard Forum Slide Show Slide #3

Who s Plane Is It? Jack Morrison s E-Racer Built 1996 Lindy Award winner OSH 2000 Over 300 hours on airframe July 19, 2007 Canard Forum Slide Show Slide #4

Who s Plane Is It? July 19, 2007 Canard Forum Slide Show Slide #5

Consulting Process Jack approached me for engineering assistance with winglet modification he had a couple of ideas Wanted blended winglet like 737-800 thought would provide drag reduction Discussed two approaches for mods settled on one Determined modification process removal of old winglets wing preparation fabrication of new winglets attachment of new winglets Ensure adequate strength/stiffness Discussed appropriate flight testing after modifications July 19, 2007 Canard Forum Slide Show Slide #6

Aerodynamics of Canard Aircraft Winglets Nominally Whitcomb winglets, BUT Not used for L/D improvement (efficiency) as on commercial airliners and gliders Merely convenient place for vertical stabs/rudders Lower winglet on LE/COZY has aerodynamic purpose, but not pertinent to this issue Intersection not optimal lots of separation drag E-Racer intersection especially nonoptimal drag-wise (looks good, though) more room for improvement with E-Racer E-Racer Long-EZ / COZY July 19, 2007 Canard Forum Slide Show Slide #7

Modification Process - #1 bar Foam July 19, 2007 Canard Forum Slide Show Slide #8

Modification Process - #2 July 19, 2007 Canard Forum Slide Show Slide #9

Aircraft Configuration - Before Standard E-Racer Airframe First flew 1996 with Chevy 4.9L V6 Supercharged engine Changed to IO-540 - Supercharged with Auto Ignition system Retractable gear per E-Racer plans Stock E-Racer winglets July 19, 2007 Canard Forum Slide Show Slide #10

Aircraft Configuration - After New Paint New Winglets That s it Easy to compare only one major aerodynamic change July 19, 2007 Canard Forum Slide Show Slide #11

Aircraft Testing Tuft Testing notice attached flow in intersection region tufts flowing straight back Speed / Performance Testing Stall Testing July 19, 2007 Canard Forum Slide Show Slide #12

Aircraft Performance RPM 2310 2410 2440 2420 2500 2500 2500 2520 Original Winglets Pre-Blend MP IAS 29.4 175 31.0 180 31.6 180 31.8 183 32.5 184 32.6 181 32.8 178 32.8 180 33.0 182 32.5 185 34.4 180 34.2 180 34.6 180 35.4 189 36.2 190 36.8 188 36.6 181 Pre-Blend TAS 179 188 186 188 189 183 183 188 189 191 186 188 188 196 195 191 190 Normalized Power (%) 68 74 76 76 78 78 79 79 79 79 82 83 83 88 90 92 92 RPM 2300 2300 2500 Blended Winglets Blended MP IAS 29.1 189 29.3 183 33.4 189 33.5 190 34.1 192 34.2 190 35.2 192 35.4 191 40.1 208 Blended TAS 192 190 199 202 199 200 201 200 215 Speed vs. Power data @ NORMALIZED power settings (NOT % power available!!!) Highest power USED in testing set to 100%, just for comparison purposes Normalized Power (%) 67 67 80 80 82 82 84 85 100 July 19, 2007 Canard Forum Slide Show Slide #13

Performance Graphs Blended winglets on E-Racer provide ~10 kt. TAS increase at equivalent power settings ~ Equivalent to wheel pants on L.E. / COZY Greater than gear leg fairings on L.E. / COZY Linear Curve fit NOT accurate, just allows for simple comparison need more data points for polynomial fit TAS TAS vs. Normalized Power 220 Pre-Blend TAS 215 Blended TAS 210 Linear (Pre-Blend TAS) Linear (Blended TAS) 205 200 195 190 185 180 175 65 70 75 80 85 90 95 100 NORMALIZED Pow er (%) July 19, 2007 Canard Forum Slide Show Slide #14

Other Performance Diffs. None No major flight characteristic changes No pitch, roll, yaw issues No stall differences July 19, 2007 Canard Forum Slide Show Slide #15

Extension to Other Canard Aircraft? LE/VE maybe Standard aircraft probably not fast enough to see much advantage Better winglet intersection than E-Racer to start with leaves less room for improvement CG issues possibly not AS sensitive to lower winglet disappearing Might be more work than it s worth, but could gain a few 2 to 4 kts. Berkut most likely candidate Fast enough to get advantage Better winglet intersection than E-Racer to start with leaves less room for improvement but CG issues possibly not AS sensitive to lower winglet disappearing Could be worth a try might gain 5 to 10 kts. COZY III/MKIV (and other 3/4-seat canards) NOT RECOMMENDED Need a great deal of experimentation on CG issues / lower winglet loss compatibility Standard aircraft probably not fast enough to see much advantage Better winglet intersection than E-Racer to start with leaves less room for improvement Probably 2 to 4 kts. max. gain Concomitant deep stall issues at the slow end due to lower winglet disappearance July 19, 2007 Canard Forum Slide Show Slide #16

Questions? (& Answers) My Email: marc_zeitlin@alum.mit.edu Jack s Email: N345JM@comcast.net My Website: http://www.cozybuilders.org/ July 19, 2007 Canard Forum Slide Show Slide #17