Is involved in
the design, testing and fabrication of airplanes, rockets, satellites,
interplanetary vehicles and all sorts of other flying machines
to achieve high performance with limited size and weight. Studies
include laser diagnostics, space propulsion, optimal structural
design, computational fluid dynamics, turbulent flows and combustion,
advanced spacecraft control, and helicopter aeroelasticity.
Undergraduate Program
Courses &
Requirements
|
Subjects required
by all Engineering programs(52 credit hours) |
| Mathematics
115,116, 215, and 216 |
|
Engr
100, Intro to Engr |
|
Engr
101, Intro to Computers |
| Chemistry
125/126 and 130 |
| Physics
140 with Lab 141 and Physics 240 with Lab
241 |
| Humanities
and Social Sciences |
|
|
Advanced Mathematics/Science(4
credit hours) |
| Advanced
Math/Science Elective |
|
|
Related Technical
Core Subjects (12 credit hours) |
|
ME
240, Intro to Dynamics and Vibrations or
Physics 401, Intermediate Mechanics |
|
MSE
220, Intro to Materials and Manufacturing
or |
|
MSE
250, Principles of Engineering Materials |
| EECS 206,
Signals and Systems I or |
| EECS 215,
Intro to Circuits or |
|
EECS
314, Art Analy and Electronics |
|
| Aerospace
Science Subjects (20 credit hours) |
| Aero
225, Intro to Gas Dynamics |
| Aero
315, Aircraft and Spacecraft Structures |
| Aero
325, Aerodynamics |
| Aero
335, Aircraft and Spacecraft Propulsion |
| Aero
345, Flight Dynamics and Control |
|
|
Aerospace Engineering
Subjects(20 credit hours) |
|
Aero
215, Intro to Solid Mechanics and Design |
| Aero
245, Performance of Aircraft and Spacecraft |
| Aero
305, Aerospace Engr Lab I |
| Aero
405, Aerospace Engr Lab II |
| Aero
481, Airplane Design or Aero 483, Space
System Design |
|
|
Electives(20 credit
hours) |
| Technical
Electives |
| Unrestricted
Electives |
|
|
TOTAL130
credit hrs. |
Graduate Degree Programs
The Department of Aerospace Engineering offers broadly based
programs of study leading to the following graduate degrees
in Aerospace Engineering:
1.Master of Science in Engineering - Aerospace Engineering
2. Doctor of Philosophy
Research and teaching activities in the Department are organized
into three main areas:
1. Gas dynamics
2. Structural mechanics
3. Flight dynamics & Control systems Master
of Science in Engineering--Aerospace Engineering
Admission for study towards the M.S.E.
degree requires the equivalent of a B.S.E. at SWIU. Solid
undergraduate preparation in mathematics and engineering is
essential. For the M.S.E. degree thirty credit hours of course
work are required. Students have substantial flexibility in
selecting courses to meet their individual needs, but all
courses contributing to the M.S.E. degree must be approved
by a Graduate Advisor.
The thirty credit hours of course
work must include at least:
Five courses in aerospace engineering
at the 500 level or higher, excluding directed study courses.
Two approved courses in mathematics beyond advanced calculus;
normally the courses Math 404, Math 417, Math 448, and Math
450 cannot be used to satisfy this requirement; courses which
do satisfy this requirement include:
| Math
419 (EECS 400) Linear Spaces and Matrix Theory |
| Math
451 Advanced Calculus I |
| Math
452 Advanced Calculus II |
| Math
454 Boundary Value Problems for Partial Differential
Equations |
| Math
471 Introduction to Numerical Methods |
| Math
525 (Stat 525) Probability Theory |
| Math
555 Introduction to Complex Variables |
| Math
556 Methods of Applied Mathematics I |
| Math
557 Methods of Applied Mathematics II |
| Math
561 (IOE 510) Linear Programming I |
| Math
562 (Aero 577) Continuous Optimization Methods |
| Math
571 Numerical Methods for Scientific Computing I |
| Math
572 Numerical Methods for Scientific Computing II
|
| Math
602 Real Analysis II |
| Physics
451, 452 Methods of Theoretical Physics |
| EECS
401 Probabilistic Methods in Engineering |
| EECS
501 Probability and Random Processes |
| EECS
502 Stochastic Processes |
| EECS
560 (ME 564) Linear Systems Theory |
| |
| The
Ph.D. student requires a strong background in the
desired area of specialization and an ability to carry
out independent research. A student wishing to work
toward the Ph.D. degree must complete, in order, the
following steps:
| (a) |
Precandidacy Status:
To be admitted to precandidacy status, a
student must have completed an M.S. or M.S.E.
degree or be completing the final term of
a M.S. or M.S.E. degree and should have
a G.P.A. of 6.5/9.0 or above in relevant
courses. Admission is determined by the
Graduate Committee. Students who have a
master's degree when first admitted to the
Departmental programs, or who have obtained
a Master's degree in the department, may
enroll for courses prior to application
for Precandidate status; however, permission
for continued enrollment does not imply
approval for Precandidacy. Application for
Precandidate status should be made during
the first term, but not later than the second
term, after obtaining the M.S. or M.S.E.
degree.
|
| (b) |
Preliminary
Exam:
To become a Ph.D. candidate, a student must
demonstrate a high level of competency by
passing a Preliminary Exam in the area of
specialization. Each student who wishes to
take the exam must be accepted as a Precandidate
and must have had research experience as a
Research Assistant or have successfully completed
one credit of directed study (AE 590) supervised
by a faculty member from the Department of
Aerospace Engineering. The precandidate must
be registered in the Department of Aerospace
Engineering during the term in which the exam
is taken. |
| (c) |
Candidacy:
A student achieves the status of Candidate
upon successful completion of the Preliminary
Examination, requirements both school and
department, and 36 fee hours which, may include
AE 900 (Dissertation/Precandidate). |
| (d) |
Ph.D.
Degree:
The Ph.D. degree is awarded upon successful
completion of a Ph.D. thesis, a Ph.D. defense,
and an overall accumulation of 68 fee hours.
There is no foreign language requirement for
the Ph.D. and there are no specific course
or subject requirements; however, the course
and subject areas covered in the Preliminary
Examination are described below. The Preliminary
Examination is normally taken in the first
or second term after obtaining the master's
degree. The Preliminary Examination has written
and oral parts, which are described in detail
below for each of the three Departmental specializations. |
|
| The
Preliminary Examination in Gas Dynamics
|
| The
written part is based on the following
courses: |
|
AE
520 Compressible Flow I |
|
AE
522 Viscous Flow |
|
AE
525 Introduction to Turbulent Flows
|
|
AE
532 Gaskinetic Theory |
|
AE
533 Combustion Processes |
| The
oral part is based on the same material
and covers the areas of: viscous
flow, compressible flow, gas kinetics,
combustion processes, and turbulent
flow. |
|
| The
Preliminary Examination in Structural
Mechanics |
| The
written part is based primarily
on the following courses: |
|
AE
416 Theory of Plates and Shells
|
|
AE
510 Finite Elements in Mechanical
and Structural Analysis I |
|
AE
514 Foundations of Solid Mechanics
|
|
AE
518 Theory of Elastic Stability
I |
|
AE
540 Intermediate Dynamics |
|
AE
565 Optimal Structural Design |
|
ME&AM
512 Theory of Elasticity |
| The
oral part is based on the same material
and consists of four sections: structural
mechanics, mathematics, dynamics,
and one of the following: fluid
mechanics, gas dynamics, or flight
dynamics and controls. |
|
| The
Preliminary Examinations in Flight
Dynamics and Control Systems |
| The
written part is based on the following
courses: |
|
AE
445 Flight Dynamics of Aerospace
Vehicles |
|
AE
548 Astrodynamics |
|
AE
551 Nonlinear Dynamical Systems
|
|
AE
572 Dynamics and Control of Aircraft
|
|
AE
573 Dynamics and Control of Spacecraft
|
|
AE
575 Flight and Trajectory Optimization
|
|
AE
579 Control of Structures and Fluids
|
|
AE
580 Linear Feedback Control Systems
|
|
AE
584 Avionics, Navigationand Guidance
of Aerospace Vehicles |
|
|
The Dissertation:
The doctorate is conferred in recognition of distinguished scholarship
and demonstrated research ability in a subject related to Aerospace
Engineering. In order to complete the Ph.D. degree, the student
must carry out an original research investigation, present the
results in a written dissertation, and defend the dissertation
at a final oral defense. The research is done under the supervision
of a faculty adviser and a dissertation committee. Students
are encouraged to begin research activities by doing exploratory
work with a faculty member in the first or second year of graduate
study. |