University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
Beam Deflection Review
(4.34.5)
MAE 316 Strength of Mechanical Components
NC State University Department of Mechanical and Aerospace Engineering
1
Beam Deflection Review
Deflection Due to Bending (4.
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
Study 6
Due date:21.12.2016
1.Calculate the amount of fuel (in terms of volume) you need from the fuel weight fraction analysis.
2. Size the wing of your airplane according to the W/S calculations and
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
AEE 451 Aircraft Design
07.11.2016
120121015  Hasan Hseyin Aydodu
120121047  Fatih Ahmet Sargl
120121605  Moumin Quran
120121010  Fettullah Arslan
130121042 Ege Konuk
TABLE OF CONTENTS
I.
II.
A.
B
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
II. Hafta
Frekans Dalm ve
Grafikleme
Neden frekans dalm oluturulur?
Veriyi gruplara ayrarak anlalabilir hale
getirmek iin
Gzlenme sklklarn ve olaslklarn
belirlemek iin
2k > n
k: snf says, n: rneklem b
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
INTRODUCTION TO AERONAUTICS: A DESIGN PERSPECTIVE
CHAPTER 6: STABILITY AND CONTROL
The balancing of a gliding or flying machine is very simple in theory. It merely consists in causing the
center of pr
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
International Journal of Aerospace Sciences 2012, 1(5): 8591
DOI: 10.5923/j.aerospace.20120105.01
Deflection of Structures Using Principle of Quasi Work
Inder Krishen Panditta* , M. Maruf Wani
M echa
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
International Journal of Control Science and Engineering 2012, 2(6): 181188
DOI: 10.5923/j.control.20120206.06
A SelfTuning Fuzzy Logic Controller for Aircraft Roll
Control System
Omur Akyazi1,* , M
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
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University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
JOURNAL OF THEORETICAL
AND APPLIED MECHANICS
47, 2, pp. 435456, Warsaw 2009
STABILITY AND LOAD CARRYING CAPACITY OF
MULTICELL THINWALLED COLUMNS OF RECTANGULAR
CROSSSECTIONS
Marian Krlak
Katarzyna
University of Turkish Aeronautical Association  Merkez Campus
statics
AEE 261

Fall 2017
Chapter 4:
Force System Resultants
PROBLEMS
Example 00
Calculate the moment of the 600N force about the base point .
Example 10
1 = 375 N
2 = 500 N
0.5 m
8m
6m
5m
3 = 160 N
Example 1I
Example 1II
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
Compare your results with the requirements.
STUDY 8 9
06.01.2017
1. Calculate the maximum speed of your airplane with and without afterburner at @ 14000 m altitude @ combat
weight.
2. Calculate th
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
Class Schedule  Spring 2017
Nuclear, Plasma, and Radiological Engineering
NPRE 402 Nuclear Power Engineering credit: 3 OR 4 hours.
Principles of utilization of fission energy in nuclear power enginee
University of Turkish Aeronautical Association  Merkez Campus
statics
AEE 261

Fall 2017
AEE 261 STATICS
Lecturer: Assoc. Prof. Dr. etin ENTRK
Email: [email protected]
Office: Faculty of Aeronautics and Astronautics Building, No. 122
Phone: +90 312 444 6173
Course Description: This is
University of Turkish Aeronautical Association  Merkez Campus
statics
AEE 261

Fall 2017
Chapter 5:
Equilibrium of a Rigid Body
PROBLEMS
Example 1I
Example 1II
80 N
5m
5m
3m
Example 1III
Example 1IV
The 10kg uniform rod is pinned at end . It is also subjected to a
clockwise couple mo
University of Turkish Aeronautical Association  Merkez Campus
statics
AEE 261

Fall 2017
Chapter 2:
Force Vectors
PROBLEMS
Example 1
Determine the magnitude of the resultant force and its direction
measured counterclockwise from the axis by using
a) the graphical method,
b) the scalar not
University of Turkish Aeronautical Association  Merkez Campus
statics
AEE 261

Fall 2017
Chapter 3:
Equilibrium of a Particle
PROBLEMS
Example 1
Example 2
Example 4
Example 6
Determine the tension in each cord and the stretch in the spring
used to support the 100kg crate shown in the fig
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
STUDY 4
Deadline is 30.11.2016
1)Obtain the thrust to weight ratio of the aircraft by using historical trend,
competitor aircraft or nonlinear regression
2) Calculate W/S for
 stall speed, (
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
_
Aircraft design project fifth study
refined estimation of design takeoff
weight of a fighter aircraft
Kksal M Danan, Sleyman M Krolu, Uur Mermer,
Mehmet S Okal and Meltem ahin
Abstract
This report i
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
T
DERS KATALOG FORMU
(COURSE CATALOGUE FORM)
Dersin Ad
Course Name
Uak Tasarm Temelleri
Principles of Aircraft Design
Kodu
(Code)
UCK 451E
Yaryl
Kredisi
AKTS Kredisi
(Semester) (Local Credits) (ECTS C
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
Study 7
Deadline is 28.12.2016 Classroom
1. Obtain and plot the lift curve slope of your aircraft as a function of the Mach number (between M=0.1 and 2.2)
at sea level.
2. Calculate the maximum lift c
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
Examples and
Problems
Problem 1.31
Chips of width L = 15 mm on a side are mounted
to a substrate that is installed in an enclosure
whose walls and air are maintained at a
temperature of Tsur = T = 25o
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
AE372 Flight Mechanics
Spring 2013, Dr. Ilkay Yavrucuk
HW#4
AE 372 Flight Mechanics
Spring 2013
Due on: May 3rd 2013 at the beginning of class.
This homework will have the we
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
College of Engineering and Computer Science
Mechanical Engineering Department
Mechanical Engineering 370
Thermodynamics
Fall 2010 Course Number: 14319
Instructor: Larry Caretto
Unit Twelve Homework So
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
Creep Compliance of a standard viscoelastic solid
The differential equation is
E1 E2
1
d
1 d
dt
E1 E2 E1 dt
Suppose (t ) 0 for all t < 0.
At time t = 0 a constant stress, (t ) 0 is applied, such t
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
AE 362
SPRING 20100321
HOMEWORK 2
(due March 31stWednesday)
1 Consider a simply supported beam of length L with an overhang length L/2. The first portion of the
beam is subjected to a uniform load
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
1
AERE355 Fall 2015 TakeHome EXAM 1 Due 9/28(M) Name_
[Note: You MUST use the homework format, or risk zero credit]
PROBLEM 1 (15pts) This problem addresses some points in Chapter 1 that some student
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
AERO 304
Objective: To review what you learned in ENGR 214 and relate it to what you are
learning in AERO 304
Conservation of Linear Momentum
Derive the following differential equations of equilibriu
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
A straight, thin, steel strip of thickness t and width w is clamped to a rigid block which is
flat up to point B and then becomes a cylinder of radius R as shown. The flexural
stiffness of the beam is
University of Turkish Aeronautical Association  Merkez Campus
aircraft structure
AEE 261

Fall 2015
Homework 1: AE302, Aircraft Propulsion Systems
September 6, 2007
Due: September 13, 2007, beginning of class
Problem 1: Chapter 2, problem 7
Problem 2:
A water jet is impinging on a curved surface as