Authors: Zhihao Chen, Zixiao Tan
This project investigates the factors affecting paper helicopter flight duration through a full factorial experimental design. We examine four factors to determine their individual and interactive effects on flight time.
- Which factors are most important for achieving longer flight duration?
- Does the rotor length effect vary by leg width?
- What is the ideal factor combination for maximum flight time?
| Factor | Low Level | High Level |
|---|---|---|
| Rotor Length | 7.5 cm | 8.5 cm |
| Leg Length | 7.5 cm | 12.0 cm |
| Leg Width | 3.2 cm | 5.0 cm |
| Leg Clip | No | Yes |
- Type: Full factorial design (2^4 = 16 treatment combinations)
- Replications: 5 flights per combination
- Total Observations: 80 flights
- Outcome: Flight time (seconds)
Rotor length is the most critical factor for flight duration:
- Positive effect: High rotor (+0.220s, p<0.001)
- Negative effects:
- Paper clip (-0.315s, p<0.001)
- High leg length (-0.159s, p<0.001)
- High leg width (-0.152s, p<0.001)
The rotor × leg width interaction is not significant (p>0.05), indicating that the rotor length effect does not vary by leg width. However, other significant interactions were found:
- rotor × leg length: -0.448 (p=0.006)
- rotor × clip: -0.490 (p=0.003)
- rotor × leg length × clip: +0.696 (p=0.003)
Treatment 'a' yields the longest flight duration:
- Configuration: High rotor (8.5cm), low leg length (7.5cm), low leg width (3.2cm), no clip
- Expected flight time: 2.47 seconds (95% CI: 2.31-2.63s)
- Strategy: Maximize the beneficial rotor effect while minimizing all detrimental factors
project2.Rmd- R Markdown analysis file with full methodology and codeproject2.pdf- Compiled PDF report with results and visualizationspaperplane.csv- Experimental flight time dataproblem.pdf- Project assignment descriptionMaking a Paper Helicopter.pdf- Helicopter construction guide
- Full factorial ANOVA model with all main effects and interactions
- Model diagnostics to verify assumptions (normality, constant variance)
- Nested F-tests to compare models
- 95% confidence intervals for treatment effects
library(tidyverse)
library(dplyr)
library(ggplot2)
library(kableExtra)- Open
project2.Rmdin RStudio - Install required packages
- Knit the document to generate the PDF report
The experiment demonstrates that longer rotor length significantly improves flight time, while adding weight (clip) or increasing leg dimensions reduces performance. The optimal helicopter design achieves approximately 2.5 seconds of flight time by maximizing rotor length and minimizing all other factors.