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The Effect of Mass of Helicopter and Length of Hanging Mass from Helicopter on Acceleration. Abby Bault – Center Line Megan Satawa – Warren Woods Tower. TABLE OF CONTENTS. Background Problem & Hypothesis Materials & Procedures Data Collected Odd Trials/Data Statistical Tests.
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The Effect of Mass of Helicopter and Length of Hanging Mass from Helicopter on Acceleration Abby Bault – Center Line Megan Satawa – Warren Woods Tower
TABLE OF CONTENTS • Background • Problem & Hypothesis • Materials & Procedures • Data Collected • Odd Trials/Data • Statistical Tests • Conclusion • Errors Made • Real World Application • Further Research • Review • Questions
BACKGROUND • Lift • Thrust • Drag • Weight
LIFT • Force that causes helicopter to move up • Bernoulli Principle • Pressure increases as speed increases • Wings • Air flows around body: changes pressure and velocity • Through center of pressure
THRUST AND WEIGHT • Thrust moves helicopter forward • Must be equal to weight • Weight is force of gravity – pulls down
DRAG • Force that opposes motion • Created by contact with fluid • Skin friction: interaction between solid and gas • Acts through center of pressure
PROBLEM • To determine the effect of mass of helicopter and distance of hanging mass from helicopter on the acceleration of the helicopter.
HYPOTHESIS • If the distance of the hanging mass from the helicopter and the mass of the helicopter are the greatest then the acceleration will be the slowest.
MATERIALS • TI-nSpire • Meter Stick • Propel RC Toy Helicopter • Craft String • Propel RC Controller • Different Masses • Video Recorder • Timing Device • 18 AA Batteries
PROCEDURES • Randomize trials and set up camera and meter sticks • Fly the helicopter and record the flight • Analyze the video using LoggerPro • Record the acceleration
OBSERVATIONS • Outline trials with specific observations HERE
ANALYSIS • Two-Factor DOE • Mass and string length
CONCLUSION • Lack of statistical significant • Based of D.O.E analysis
CONCLUSION • Scientifically significant results • Based on dot plot of effects Distance Mass
CONCLUSION • Hypothesis: Accepted
ERRORS MADE • Wrong weight on helicopter for DOE 1 • Trials redone • Lack of operating experience
Design Flaws • Inconsistent helicopter battery power
FURTHER RESEARCH • Different types of helicopters • Different factors • Humidity, air flow(turbulent or laminar) • jkda
real world application • MedEvac Flights • Emergency Rescue