MIDDLE EAST TECHNICAL UNIVERSTY AEROSPACE ENGINEERING DEARTMENT

AE451

AERONAUTICAL ENGINEERING DESIGNTEAM # and NAME

Project: Write down project title

STUDY #

NAME ID Contribution

Instructor : Prof. Dr. Dilek Funda Kurtuluş

Assistant :

Due Date : …/…/2018

An image related to project or study

AE 451 Team # Study # Due Date: .../.../2018

ABSTRACT

Summaries what have been done in the study and explain shortly how

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TABLE OF CONTENTS

Abstract…………………………………………………………………………………..i

Table of Contents…...……………………………………………………………………ii

1. INTRODUCTION….………………………………………………………………..12. WEIGHT

ESTIMATION……………………………………………………………………….2

2.1 Empty weight…………………………………………………………………………3

3. CONCLUSION………………………………………………………………………30

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MIDDLE EAST TECHNICAL UNIVERSTY AEROSPACE ENGINEERING DEARTMENT

1. INTRODUCTION

Do not change font size and type. In the ıntroduction part explain the methods that is used in the study make citations from reference books and reports

2. WEİGHT ESTIMATION

Also figures and tables that is used in the report must be referred in the text. Figure 1 shows how should a figure placed to the report. All Figures should be centered the page and maximum width of the figure should be less than or equal to 16 cm.

Figure 1 Each figure should be explained properly in the text [1]

If the figure is taken from a web site put the reference at the Reference section as is shown for Ref. [1] and Figure 1.

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AE 451 Team # Study # Due Date: .../.../2018

2.1 Tables

Now, Table name should be written on top of the table as seen in Table 1. Use simple and less fancy tables.

Table 1 Robot-Wings motion limits

with Load Cell without Load Cellθ1 ∓90  0 ∓180  0

θ2 +450/−900 +450 /−2250

θ3 ∓180  0 ∓180  0

(θ̇1)max . 1600/ s(θ̇2)max. 2900/ s(θ̇3 )max. 2900/ s

2.2 Equations

All equations that are used in the calculations should be given and numbered properly. Eqn. 1 is shows how to write an equation properly. Also, do not forget referring the equation with in the text.

ψ (ε )=0 , ε ≤ ε0

ψ1 , ε ≤ ε1

K p ε , ε>ε1

(Eq. 1)

Graphs are pretty important. First of all, each graph should have a proper name. Then, axes titles should be written with the units. Furthermore, do not forget to add legend to the graphs. Figure 2 presents a fairly good graph.

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0 2 4 6 8 10 12 14 16 18 20-20

-15

-10

-5

0

5

10

15

20

Plunge Axis P-Constant Calibration Test

Desired Experimental Kp=4.2

Time [s]

Positi

on [d

eg]

Figure 2 Plunge axis P-Constant calibration test data

2.3 How to make citations

Recent advances in the microelectronics technology enables the production of smaller UAV systems that are called Micro-UAV [2]. Firstly, dynamic stall of the wing creates strong leading edge vortex (LEV), second is the wake capturing phenomenon as explained by Dickinson et al. [3], and the last one is the clap-and-fling mechanism for the tandem wing cases[4]. Robotic flapping mechanism presented in this paper, which is instrumented with load and torque sensors, makes possible the investigation of lift-generating mechanisms. Robot-Wings has two independent wings that enables to create different flapping trajectories composed of sinusoidal, step and ramp functions.

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AE 451 Team # Study # Due Date: .../.../2018

3. CONCLUSION

Come up with a conclusion and mention about the future woks.

ACKNOWLEDGEMENT

If any kind of help has been taken from a person, his/her efforts should be kindly acknowledged.

References

[1] https://www.tu-braunschweig.de/ifl/forschung/flugzeugvorentwurf/index.html;jsessionid=TRIFORK491364216530

[2] Birch, J.M., Dickinson, M.H., The influence of wing–wake interactions on the production of aerodynamic forces in flapping, flight. J Exp. Biol., 206:2257–2272, 2003

[3] Dickinson, M.H., Götz, K.G., Unsteady aerodynamic performance of model wings at low Reynolds numbers, J Exp. Biol., 174:45–64, 1993

[4] Weis-Fogh, T., Quick estimates of flight fitness in hovering animals, including novel mechanism for lift production. J Exp. Biol., 59:169–230, 1973

Appendix

If there are additional equations that you want to show please put in Appendix

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