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