Curriculum in Aerospace Engineering
Aerospace engineering is a diverse and
rapidly changing field which includes aerodynamics, structures
and materials, propulsion, dynamics and control, and astrodynamics.
The primary application of aerospace engineering is to the design
and development of flight vehicles such as aircraft, missiles,
spacecraft and satellites; but aerospace engineering is also
important and applicable to other vehicles and systems such as
submarines, automobiles, trains, trucks, buses and rapid transit.
The objectives of the Aerospace Engineering
program are: (1) using a high quality faculty, provide a comprehensive
aerospace engineering education that develops in students the
fundamental skills necessary for the design, synthesis, analysis
and research development of aircraft, spacecraft and other high
technology flight systems; and (2) prepare students for the aerospace
engineering profession and related fields by developing in them
the attributes needed so that they can contribute successfully
to society and to the engineering profession now and in the future.
The curriculum is generally composed
of three topical areas: humanities and social sciences, basic
science and mathematics, and engineering science and design.
The humanities and social science courses are intended to broaden
a student's education and to provide training in oral and written
communication skills. In addition, they ensure a liberal education
and an awareness of our cultural heritage and contemporary human
situation. The basic science and mathematics courses provide
the necessary foundation for the engineering science courses.
The latter start at the sophomore year with topics common to
many fields of engineering and continue in the last two years
with sequences in aerodynamics, structures and materials, propulsion,
and dynamics and control. These provide a strong fundamental
basis for advanced study and specialization, while technical
electives offer a concentration of study in fields of special
interest. Design philosophy and practice are developed throughout
the curriculum so as to relate analysis to aerospace engineering
design; and the design of aerospace system components is particularly
emphasized in the junior- and senior-level courses. A senior-level
design sequence, involving specific goals, objectives, and constraints,
integrates analysis and design tools and requires students working
in small teams to design an aerospace system such as an aircraft,
rocket or spacecraft. Application of computers and computational
methods is required and emphasized in all courses.
The department's laboratories are among
the best in the nation and are used to supplement theoretical
studies in the major disciplines. There are several water and
wind tunnels for low-speed and supersonic aerodynamic studies,
a jet engine test facility, numerous research aircraft, a flight
simulator, and state-of-the-art materials and structures testing
equipment--all equipped with modern instrumentation. The department,
as well as the University, provides an extensive array of computing
resources, including PCs, workstations and mainframe systems.
The department participates in the Cooperative
Education Program which provides an opportunity for qualified
students to obtain practical engineering work experience with
participating companies. The co-op degree plan includes three
or four work periods which are integrated with full-time study
semesters.
The department also offers programs of
study leading to the M.Eng., M.S. and Ph.D. degrees (see Texas
A&M University Graduate Catalog ).
Sophomore Year
|
First Semester |
(Th-Pr)
|
Cr
|
|
Second Semester |
(Th-Pr)
|
Cr
|
|
AERO 201 Intro. to Aerospace Engr. |
(3-0)
|
3
|
|
AERO 320 Numerical Methods |
(2-3)
|
3
|
|
ENGR 211 Conserv. Prin. of Engr.
Mech |
(2-2)
|
3
|
|
ENGR 213 Prin. of Materials Engr. |
(2-2)
|
3
|
|
ENGR 212 Conserv. Prin. in Thermal
Sci. |
(2-2)
|
3
|
|
ENGR 214 Conserv. Principles in Continuum
Mechanics |
(2-2)
|
3
|
|
MATH 251 Engineering Mathematics
III |
(3-0)
|
3
|
|
ENGR 215 Principles of Electrical
Engr. |
(2-2)
|
3
|
|
Electives |
|
6
|
|
MATH 308 Differential Equations |
(3-0)
|
3
|
|
|
|
18 |
|
|
|
15 |
Junior Year
|
AERO 301 Theoretical Aerodynamics |
(3-0)
|
3
|
|
AERO 303 High Speed Aerodynamics |
(3-0)
|
3
|
|
AERO 302 Aerospace Lab. I |
(1-3)
|
2
|
|
AERO 305 Aerospace Lab. II |
(1-3)
|
2
|
|
AERO 304 Structural Analysis I |
(4-0)
|
4
|
|
AERO 306 Structural Analysis II |
(3-0)
|
3
|
|
AERO 310 Aerospace Dynamics |
(3-0)
|
3
|
|
AERO 351 Aerothermo. and Propulsion |
(3-0)
|
3
|
|
Technical writing |
|
3
|
|
AERO 421 Dynamics of Aerospace |
|
|
|
Elective |
|
3
|
|
Vehicles |
(3-0)
|
3
|
|
|
|
18 |
|
Science elective |
|
3
|
|
|
|
|
|
|
|
17 |
Senior Year
|
AERO 401 Aerospace Vehicle Design
I |
(2-3)
|
3
|
|
AERO 402 Aerospace Vehicle Design
II |
(0-6)
|
2
|
|
AERO 423 Space Technology I |
(3-0)
|
3
|
|
AERO 452 Heat Transfer and Viscous
Flows |
(3-0)
|
3
|
|
Computational Methods/Mathematics |
|
3
|
|
ENGR 482 Ethics and Engineering |
(2-2)
|
3
|
|
Design elective |
|
3
|
|
Technical electives |
|
5
|
|
Technical elective |
|
3
|
|
Elective |
|
3
|
|
|
15
|
|
|
|
16
|