Assignment 3_fractional factorial

docx

School

Conestoga College *

*We aren’t endorsed by this school

Course

8115

Subject

Industrial Engineering

Date

Feb 20, 2024

Type

docx

Pages

9

Uploaded by CommodoreSteelHedgehog34

Report
Assignment 3: Fractional Factorial Parth. M. Patel Harshit Mistry Parth Bhuva Kushal Patel Santosh Prajapati Milan Patel Urvil Patel Amalsha Process Quality Engineering – Conestoga College QUAL 8115: Advance Design of Experiments Iain Hastings July 14, 2023
Executive Summary The helicopter experiment identifies the factors affecting the helicopter's flight falling time. On a scale of 1 to 10, the flight quality is evaluated based on two factors: the falling time and the fall quality. We analyze the experimental design using 1/8 fractional factorial because there are 7 factors with 2-factor levels. Based on the study, it was evident that factors influencing the flight, the rotor length, tail length, tail width, paper width, and wing fold, are of high quality in this case. Experimental recipe: To examine the factors which affect the flight time and flight quality of paper helicopters. Objective statement: Through this experiment, we want to find the best helicopter performance according to falling time and falling quality. Response: Helicopter time Factors: 7 factors (Overall width, Rotor length, Tail length, Tail width, Paper type, Paper clip, Point tail) Levels of Factors: Each factor with two-level Experimental design: 1/8 fractional factorial design (no replicates).
Data StdOr der RunOr der Cente rPt Block s over all widt h Rotar lengt h Tail Lengt h Tail widt h Pape r type Pape r clip Point tail Time Quali ty 6 1 1 1 90 105 105 32 Light yes No 2.32 8 2 2 1 1 90 105 102 32 Heav y No Yes 1.2 5 7 3 1 1 82 107 105 32 Light No Yes 2.5 8 16 4 1 1 90 107 105 36 Heav y yes Yes 1.4 5 5 5 1 1 82 105 105 32 Heav y yes Yes 1.05 4 12 6 1 1 90 107 102 36 Light No No 1.9 6 13 7 1 1 82 105 105 36 Heav y No No 1.52 5 11 8 1 1 82 107 102 36 Heav y No Yes 1.62 5 15 9 1 1 82 107 105 36 Light yes No 2.1 7 3 10 1 1 82 107 102 32 Heav y yes No 1.9 6 9 11 1 1 82 105 102 36 Light yes Yes 2.15 7 1 12 1 1 82 105 102 32 Light No No 1.88 6 10 13 1 1 90 105 102 36 Heav y yes No 1.4 5 8 14 1 1 90 107 105 32 Heav y No No 1.6 5 14 15 1 1 90 105 105 36 Light No Yes 3.18 9 4 16 1 1 90 107 102 32 Light yes Yes 2.3 8
Your preview ends here
Eager to read complete document? Join bartleby learn and gain access to the full version
  • Access to all documents
  • Unlimited textbook solutions
  • 24/7 expert homework help
Full model analysis: As per the analysis of variance and Pareto chart, only one factor (paper type) and one interaction (rotor length*tail width) significant. The remaining other factors and interactions are not significant.
Reduced model Analysis This reduced model was obtained by removing the non-significant terms from the full model analysis by using the 'Stepwise approach.' Here, overall width, rotor length, tail length, and tail width is not significant, but two interactions (overall width*rotor length, overall width*tail length, and rotor length*tail width) are significant. So, all non-significant factors are considered. Examine of the residual plot
As per the normality residual plot, all points are near the red line except last point which means our data is normal. From the residual versus fitted graph, one can see that the data is unevenly distributed. So, our model is best fitted (adequate). As per the model summary, the R-sq value indicates 93.30% of the model variation. Also, the R- sq(pred) value of 65.01% defines the ability of the model to predict the response. Main effect plot: As per the main effect plot, there is one factor (paper type) that is not parallel to the center line, which means, the paper type is a significant factor while falling the helicopter. There are other factors like overall width, Rotar length, Tail length, and Tail width parallel to the center line, which means they all are not significant.
Your preview ends here
Eager to read complete document? Join bartleby learn and gain access to the full version
  • Access to all documents
  • Unlimited textbook solutions
  • 24/7 expert homework help
The flight meantime is high when overall width (90mm), Rotor length (107mm), Tail length (105mm), Tail width (36mm), and paper type (light). Examine the interaction plot. As per the interaction plot, one can see that overall width*rotor length, overall width*tail length, and rotor length* tail width are significant. Mathematical model %SS: As per the regression equation, falling time depends on overall width, rotor length, tail width, paper type, and interaction of overall width*rotor length, overall width*tail length, and rotor length*tail width.
Analysis of Variance Source DF Adj SS P-Value     overall width 1 0.02102 0.47%     Rotar length 1 0.02402 0.54%     Tail Length 1 0.10890 2.44%     Tail width 1 0.01690 0.38%     Paper type 1 2.75560 61.86%     overall width*Rotar length 1 0.36602 8.22%     overall width*Tail Length 1 0.27040 6.07%     Rotar length*Tail width 1 0.59290 13.3% Error 7 0.29820   6.70% Total 15 4.45397   From the analysis of variance, the highest contribution is paper type(61.86%), overall width (0.47%), rotor length (0.54%), tail length (2.44%), tail width (0.38%), the interaction of width*rotor length (8.22%), overall width*tail length(6.07%) and rotor length*tail width (13.3%). Some issues while doing the experiment: Human error is common while measuring falling flight, like different releasing technique and releasing point is different in every run. Atmosphere conditions also affect this experiment, especially wind speed. Recommendation: The experiment can be done by a two replicate, which reduces the variation and increase the accuracy of result. The experiment can be done by two persons. Conclusion: From the design of the experiment, the factors that affect the dropping time of flight are paper type and interaction of overall width*rotor length, overall width*tail length, and rotor length*tail width. The maximum dropping time one can be obtained by setting of overall width (90mm), rotor length (105mm), tail length (107mm), tail width (36mm), and light paper type with no clip.
References (n.d.). Topic 8 Fractional Factorial Designs . Econestoga. https://conestoga.desire2learn.com/d2l/le/content/761431/viewContent/15909800/View
Your preview ends here
Eager to read complete document? Join bartleby learn and gain access to the full version
  • Access to all documents
  • Unlimited textbook solutions
  • 24/7 expert homework help