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Design og h.t for uav
1. Detail design of empennage of an unmanned aerial vehicle
Md. Samad Sarker, Shoyon Panday, Md Rasel, Md. Abdus Salam, Kh. Md. Faisal, and Tanzimul Hasan Farabi
Citation: AIP Conference Proceedings 1919, 020033 (2017); doi: 10.1063/1.5018551
View online: https://doi.org/10.1063/1.5018551
View Table of Contents: http://aip.scitation.org/toc/apc/1919/1
Published by the American Institute of Physics
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2. Md. Samad Sarker1,a), Shoyon Panday2), Md Rasel3), Md. Abdus Salam4), Kh. Md. Faisal5), Tanzimul Hasan Farabi 6)
1, 3, Student, Department of Aeronautical Engineering, Military Institute of Science and Technology
4, Professor, Department of Aeronautical Engineering, Military Institute of Science and Technology
5, Assistant Professor, Department of Aeronautical Engineering, Military Institute of Science and Technology
2, 6 Lecturer, Department of Aeronautical Engineering, Military Institute of Science and Technology
Email: samad.sarker@yahoo.coma
,
Proceedings of the 1st International Conference on Mechanical Engineering and Applied Science (ICMEAS 2017)
AIP Conf. Proc. 1919, 020033-1–020033-9; https://doi.org/10.1063/1.5018551
Published by AIP Publishing. 978-0-7354-1611-6/$30.00
020033-1
3. Taper ratio (
Sweep angle (
Dihedral angle (
Taper ratio (
Sweep angle (
Dihedral angle (
dyc
S
c
b
…………………….. (1)
dy
c m
fD
HV
optl
f
H
c
D
SVc
k ………………….. ………………. (2)
m
020033-2
5. to
e to
cgmC mC mC ………………… (4)
alconvention
emC
e
mC …………………… (5)
emC t
LH CV ………………… (6)
t
e
LH
m
CV
C
…………………. (7)
= Control effectiveness parameters
LC
rad
at AOA
t
LC
w
L
L
AR
C
C
020033-4