Design of a Dawn Mulvihill Competition Model Airplane - PowerPoint PPT Presentation

1 / 18
About This Presentation
Title:

Design of a Dawn Mulvihill Competition Model Airplane

Description:

Title: 30 Minute Dawn Mulvihill Author: Daniel Heinrich Last modified by: Daniel Heinrich Created Date: 11/21/2003 10:53:44 PM Document presentation format – PowerPoint PPT presentation

Number of Views:165
Avg rating:3.0/5.0
Slides: 19
Provided by: Daniel1497
Category:

less

Transcript and Presenter's Notes

Title: Design of a Dawn Mulvihill Competition Model Airplane


1
Design of a Dawn Mulvihill Competition Model
Airplane
  • Presented by
  • Jacob Gomez
  • And
  • Daniel Heinrich
  • Advisor
  • Professor Fazal B. Kauser, P.E.

2
Overview
Design and construction of an elastic powered,
free-flight, model airplane conforming to the
rules of Dawn Mulvihill.
3
Introduction
  • More from less.
  • Flying for time.
  • Elastic powered.

4
Introduction
  • Dawn Mulvihill
  • Absence of thermals
  • Most efficient model wins

5
Purpose
  • Maximum utilization of energy
  • 1/8 inch rubber strip power source
  • Dawn Mulvihill Classification
  • Double the existing high time

6
Dawn Mulvihill
  • Must be rubber strip powered
  • Projected wing area under 300 in²
  • No maximum flight time
  • Models flown at 700AM

7
Rationale
  • Indoor models fly for more than one hour
  • Indoor models have limited ceiling
  • Outdoor models have virtually unlimited ceiling
  • Outdoor times 25 of indoor times

8
Hypothesis
  • Current designs not at maximum efficiency.
  • 30 minute flight times should be attainable.
  • Utilization of energy.
  • Maximization of thrust.

9
Research
  • Most research passed on orally
  • Current designs evaluated
  • Interviewed the Top Guns of Mulvihill.
  • The canard proven more efficient

10
Methods to Achieve Goal
  • Aircraft Design
  • Testing Equipment
  • Evaluation and Analysis of Data
  • Flight Testing

11
Design
12
Equipment - testing
13
Generated Torque Curves
14
Equipment - flying
  • Winding stooge.
  • Stretch winding.
  • Efficient winding.

15
Evaluation and Analysis
  • Selection of motor with most linear torque curve.
  • Matching propeller design to torque output.
  • Allowing the propeller to operate in a narrower
    band of torque values.
  • Propellers of varying design and initial pitch
    settings.

16
Flight Testing
  • 3 Models to be constructed
  • First model approximately 170 in²
  • Second model full size with standard prop
  • Third model full size with optimal prop

17
Time Table (rev 1)
  • Project began in August 2003 with design and
    evaluation process. Table is subject to revision.

18
Closing Thoughts
Write a Comment
User Comments (0)
About PowerShow.com