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Aerospace Engineering and
Engineering Mechanics
In the College of Engineering
Office: Engineering 308
Telephone: (619) 594-6074
The undergraduate degree in Aerospace Engineering is accredited
by the Accreditation Board for Engineering and Technology, Inc.
Emeritus: Faulkner, Shutts
Chair: Plotkin
Professors: Conly, Dharmarajan, Katz, Narang, Nosseir, Pierucci, Plotkin, Wang
Associate Professor: Lyrintzis
Doctor of Philosophy degree in applied mechanics.
Master of Science degree in aerospace engineering.
Major in aerospace engineering with the B.S. degree.
No credit will be given for upper division engineering coursework taken at an institution having an engineering program which has not been accredited by the Accreditation Board for Engineering and Technology, Inc., unless the student successfully completes the first 12 units of engineering work attempted at this university. At that time, and upon recommendation of the department, credit will be given for the unaccredited work.
Students will complete a minimum of 50 units in General Education, to include a minimum of nine upper division units taken after attaining junior class standing. No more than twelve units may be used for General Education credit from any one department or academic unit.
- I. Communication and Critical Thinking: 9 units
- 1. Oral Communication (3 units)
- 2. Composition (3 units)
- 3. Intermediate Composition and Critical Thinking (3 units)
- II. Foundations: 29 units
- A. Natural Sciences and Quantitative Reasoning (17 units):
- 1. Physical Sciences (11 units)
Engineering students will take Chemistry 200 which
includes a laboratory (5 units).
- Physics 195 (3 units)
- Physics 196 (3 units)
- 2. Life Sciences (3 units)
- 3. Laboratory (satisfied under A.1. above)
- 4. Mathematics/Quantitative Reasoning
Engineering students will take Mathematics 150 (3 units)
applicable to General Education.
- B. Social and Behavioral Sciences (3 units)
- C. Humanities (9 units)
Complete three courses in three different areas. One of these
courses and the one under IV.A. below must be taken in the
same department.
- III. American Institutions: Three units of the six units of coursework which meet the American Institutions graduation requirement may be used in General Education, excluding courses numbered 500 and above.
- IV. Explorations: Total 9 units; must include one course of cultural diversity.
- A. Upper division Humanities (3 units)
Three units must be taken from the same department as one of
the Humanities courses selected in Foundations.
- B. Upper division Humanities (3 units from a department not
selected in A above.)
- C. Upper division Social and Behavioral Sciences (3 units)
The Department of Aerospace Engineering and Engineering Mechanics offers a rigorous and balanced education which includes the study of aerodynamics, aerospace structures, propulsion, flight mechanics and vehicle design. The goal of this program is to create professional aerospace engineers with an understanding of the physical fundamentals underlying atmospheric and space flight, and with the capability of applying this knowledge for research, analysis, and design purposes. Moreover, the physical background and design synthesis that are characteristic of an aerospace engineering student's education also prepare the student to work productively in other fields such as energy, transportation, and ocean engineering.
The aerospace industry, the second largest industry in our country, is one of the largest employers of engineers. Opportunities for employment in entry level positions in large aircraft companies, general aviation manufacturers, the airlines, or government aerospace-related laboratories are good. Graduates of the program are also qualified to continue their formal education at the graduate level or to accept entry level positions in several nonaerospace fields.
Students majoring in Aerospace Engineering must include in their program a sequence of fundamental courses. In addition, the students have the opportunity to satisfy their particular areas of interest by selecting a pattern of study indicated in the sequence below. This pattern includes typical aerospace engineering topics, such as aerospace vehicle design, performance, structural analysis, aerodynamics, and propulsion. The students' choice of elective courses and area of specialization must be made in consultation with their adviser and documented by the filing of an approved master plan during the first semester of their junior year.
Upper Division Writing Requirement. Departmental screening in Aerospace Engineering 303, or passing the University Writing Examination, or completing one of the approved writing courses with a grade of C (2.0) or better.
NOTE: See following page for recommended sequence of courses for the major in aerospace engineering.
123. The Aerospace Engineer (1)
Introduction to professional aerospace engineering. Emphasis on aeronautics and astronautics.
301. Low Speed Aerodynamics (3)
Prerequisite: Credit or concurrent registration in Engineering
Mechanics 340.
Subsonic flow, airfoil and wing theory, experimental characteristics of wing sections, high lift devices.
302. High Speed Aerodynamics (3)
Prerequisites: Aerospace Engineering 301 and Mechanical Engineering 352.
Supersonic flow, two- and three-dimensional compressible flow, wings in compressible flow, two- and three-dimensional method of characteristics, transonic flow.
303. Experimental Aerodynamics (2)
One lecture and three hours of laboratory.
Prerequisites: Engineering Mechanics 341 and credit or concurrent
registration in Aerospace Engineering 301. Proof of completion of
prerequisite required for the following: To be eligible for the departmental upper division writing test in this class, students must have
completed 60 units, fulfilled the Writing Competency requirement, and
completed the General Education requirement in Written Communication. Test scores or verification of exemption; copy of transcript or
enrollment confirmation.
Operating characteristics of subsonic and supersonic wind tunnels. Aerodynamic characteristics of wings and bodies. Flow visualization techniques. Force, moment and pressure distribution measurement. Use of hot-wire anemometer and schlieren equipment.
310. Aerospace Structural Analysis (3)
Prerequisite: Civil Engineering 301.
Methods of static structural analysis of problems encountered in flight of aerospace vehicles.
320. Aerospace Flight Mechanics (3)
Prerequisites: Engineering Mechanics 220 and Engineering 280.
Aerodynamics and dynamics of ballistic missiles; guidance systems; orbits and space trajectories; effects of aerodynamics, mass, rotation and shape of the earth on ballistic and space trajectories. Computer programming and problem solutions will be emphasized.
403. Aerospace Engineering Senior Project (3)
One lecture and six hours of laboratory.
Prerequisites: Aerospace Engineering 302, 303, Engineering
Mechanics 340.
Design and build an aerospace project, conduct experimental measurements, perform analyses of measured data.
410. Aerospace Structural Dynamics (3)
Prerequisites: Credit or concurrent registration in Aerospace Engineering 310.
Methods of structural dynamic analysis of problems encountered in aerospace vehicles.
430. Aircraft Propulsion Systems (3)
Prerequisite: Aerospace Engineering 302 or Mechanical Engineering 450.
Theory and performance characteristics of aircraft propulsion systems including reciprocating engines, turbojets, ramjets, etc.
440. Aircraft Stability and Control I (3)
Prerequisite: Aerospace Engineering 303.
Static stability and control, general equations of unsteady motion, stability derivatives, stability of uncontrolled motion, response of aircraft to actuation of controls.
460A. Aerospace Engineering Applications (2) I
Six hours of laboratory.
Prerequisites: Aerospace Engineering 302, 303 and 310.
Student projects in aerospace design.
460B. Aerospace Engineering Applications (3) II
One lecture and five hours of design activity.
Prerequisite: Aerospace Engineering 460A.
Student projects in aerospace design.
480. Aeroelasticity and Acoustics (2)
Prerequisites: Aerospace Engineering 302 and 410.
Theory of fluid-structure interaction. Flutter phenomena. Buffeting. Oscillating airfoils in compressible flow. Theory of acoustics. Acoustic radiation. Effect of fluid motion.
496. Advanced Aerospace Engineering Topics (1-3) I, II
Prerequisite: Consent of instructor.
Modern developments in engineering. See Class Schedule for specific content. Maximum credit six units for any combination of Aerospace Engineering 496 and 499.
499. Special Study (1-3) I, II
Prerequisite: Consent of instructor.
Individual study. Maximum credit six units for any combination of Aerospace Engineering 496 and 499.
Fall Semester Units Spring Semester Units
Chem. 200, General Chemistry 5 Phys. 195, Principles of 3
Physics
Math. 150, Single Variable Math. 151, Calc. and Anal.
Calculus 5 Geom. 4
General Education 6 ME 190, Engineering Drawing 2
AE 123, The Aerospace Engineer 1 Engr. 120, Engr. Problem 2
Analysis
General Education 6
17 17
SOPHOMORE YEAR
Fall Semester Units Spring Semester Units
Math. 252, Multivariable Phys. 197, Principles of
Calculus 4 Physics 3
EM 200, Statics 3 EE 204, Principles of Elec. 3
Engr.
General Education 9 EM 220, Dynamics 3
Phys. 196, Principles of Engr. 280, Methods of
Physics 3 Analysis 3
General Education 3
ME 260, Engineering Materials 3
19 18
JUNIOR YEAR
Fall Semester Units Spring Semester Units
ME 352, Thermodynamics and Heat Engr. 510, Methods of
Transfer 3 Analysis 3
AE 301, Low Speed Aerodynamics 3 AE 302, High Speed 3
Aerodynamics
CE 301, Intro. to Solid AE 303, Experimental
Mechanics 3 Aerodynamics 2
CE 302, Solid Mechanics Lab. 1 AE 310, Aerospace Struc. 3
Anal.
EM 340, Fluid Mechanics 3 AE 320, Aerospace Flight 3
Mech.
EM 341, Fluid Mechanics Lab. 1 General Education 3
General Education 3
17 17
SENIOR YEAR
Fall Semester-All Specializations
Units
AE 403, Aerosp. Engr. Senior Project 3
AE 410, Aerospace Struc. Dynamics 3
AE 430, Aircraft Propulsion Systems 3
AE 440, Aircraft Stab. and Control I 3
AE 460A, Aerosp. Engr. Applications 2
American Institutions 3
17
Spring Semester-All Specializations
Aerodynamics Units Aerospace Units Propulsion & Units
Structures Flight Mechanics
AE 460B, Aerosp. AE 460B, Aerosp. AE 460B, Aerosp.
Engr. Applications 3 Engr. Applications 3 Engr. Applications 3
AE 480, AE 480, AE 480,
Aeroelasticity & 2 Aeroelasticity & 2 Aeroelasticity & 2
Acoustics Acoustics Acoustics
American American American
Institutions 3 Institutions 3 Institutions 3
General Education 3 General Education 3 General Education 3
Spring Semester-According to Specialization
Choose any two courses: Choose any two courses: Choose any two courses:
AE 530, Rocket & AE 540, Arcrft. AE 520, Int.
Space Propulsion 3 Stability & Control 3 Aerospace Flight 3
II Mech.
AE 550, Viscous Flow 3 EM 510, Fin. Ele. 3 AE 530, Rocket & 3
Meth. Aero. Struc. Space Propulsion
EM 510, Fin. Elem. EM 530, Composite AE 540, Arcrft.
Meth. Aero. Struc. 3 Struc. Analysis 3 Stability & Cntrl. 3
II
17 17 17
Other electives may be substituted with permission of the adviser and department chair.
520. Intermediate Aerospace Flight Mechanics (3)
Prerequisite: Aerospace Engineering 320.
A continuation of Aerospace Engineering 320 to include orbit determination techniques, general and special perturbations, artificial satellites, rocket dynamics and transfer orbits, earth-moon trajectories, and interplanetary trajectories.
530. Rocket and Space Propulsion (3)
Prerequisite: Aerospace Engineering 430.
Equilibrium combustion thermodynamics. Performance of rocket propelled vehicles. Rocket propulsion fundamentals. Topics in chemical (solid and liquid) and electrical propulsion systems.
540. Aircraft Stability and Control II (3)
Prerequisite: Aerospace Engineering 440.
Dynamic stability and control of rigid aircraft; general equations of unsteady motion, stability derivatives, perturbed state thrust forces and moment, special problems in dynamic stability and response.
550. Viscous Flow (3)
Prerequisites: Credit or concurrent registration in Engineering
Mechanics 340, and Engineering 510.
Kinematics of fluid motion. Conservation of mass, momentum, and energy. Navier-Stokes equations; exact solutions. Boundary layer approximations, turbulent flow.
596. Advanced Aerospace Engineering Topics (3)
Prerequisite: Consent of instructor.
Modern developments in aerospace engineering. See Class Schedule for specific content. Maximum credit of six units for any combination of Aerospace Engineering or Engineering Mechanics 496, 499, and 596 applicable to a bachelor's degree. Maximum combined credit of six units of Aerospace Engineering or Engineering Mechanics 596 and 696 applicable to a 30-unit master's degree.
200. Statics (3) I, II
Prerequisites: Physics 195 and credit or concurrent registration in
Mathematics 151.
Force systems, equilibrium, structures, distributed forces, friction, virtual work, moments of inertia, vector algebra.
202. Mechanics for Electrical Engineers (3) I, II
Prerequisites: Physics 195 and credit or concurrent registration in
Mathematics 151.
Essentials of mechanics of particles and rigid bodies, for engineering applications. Emphasis on particle dynamics. Intended for Electrical Engineering majors. Not open to students with credit in Engi-neer-ing Mechanics 200 or 220.
220. Dynamics (3) I, II
Prerequisite: Engineering Mechanics 200 with a grade of C or better.
Kinetics of a particle; central force motion; systems of particles; work and energy; impulse and momentum; moments and products of inertia; Euler's equations of motion; vibration and time response; engineering applications.
296. Experimental Topics (1-4)
Selected topics. May be repeated with new content. See Class Schedule for specific content. Limit of nine units of any combination of 296, 496, 596 courses applicable to a bachelor's degree.
340. Fluid Mechanics (3) I, II
Prerequisites: Engineering Mechanics 220 or 202; and credit or
concurrent registration in Engineering 280.
Fluid statics. Laminar and turbulent flow of liquids and gases in pipes, nozzles, and channels. Dimensional analysis and modeling. Drag forces on moving or immersed objects.
341. Fluid Mechanics Laboratory (1) I, II
Three hours of laboratory.
Prerequisite: Credit or concurrent registration in Engineering
Mechanics 340.
Flow measuring devices. Experimental applications of continuity, Bernoulli and momentum equations. Model studies. Pipe and channel flows. Flow visualization techniques. Operating characteristics of wind tunnel and water table.
496. Advanced Engineering Mechanics Topics (1-3) I, II
Prerequisite: Consent of instructor.
Modern developments in engineering mechanics. See Class Schedule for specific content. Maximum credit six units for any combination of Engineering Mechanics 496, 499, and 596.
499. Special Study (1-3) I, II
Prerequisite: Consent of instructor.
Individual study. Maximum credit six units for any combination of Engineering Mechanics 496, 499, and 596.
510. Finite Element Methods in Aerospace Structures (3)
Prerequisite: Aerospace Engineering 410.
Static and dynamic analysis of aerospace structures utilizing finite element methods.
530. Composite Structural Analysis (3)
Prerequisites: Engineering 280 and Civil Engineering 301.
Strength of composite materials; lamination theory; strength analysis of laminates; bending, buckling, and vibration of composite plates.
596. Advanced Engineering Mechanics Topics (1-3)
Prerequisite: Consent of instructor.
Modern developments in engineering mechanics. See Class Schedule for specific content. Maximum credit of six units for any combination of Engineering Mechanics 496, 499, and 596 applicable to a bachelor's degree. Maximum combined credit of six units of Engineering Mechanics 596 and 696 applicable to a 30-unit master's degree.
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