MASTER OF SCIENCE DEGREE IN AERONAUTICAL ENGINEERING

Aeronautical Engineering Department Office
Engineering Bldg. (13), Room 260
(805) 756-2562 FAX: (805) 756-2376

General Characteristics

The Master of Science program in Aeronautical Engineering prepares the student for entry into a well established field of aeronautical engineering. In addition, the subject matter relative to flight simulation and controls, structures, and aerother mal sciences has been integrated into the program. The M.S. program in Aeronautical Engineering emphasizes engineering science and research activity. The degree increases a student's capability for more complex research, development, and innovative design , and prepares the student for future graduate study in engineering, leading to the Doctor of Engineering or Ph.D. degree.

Prerequisites

For admission as a classified graduate student, an applicant must hold a bachelor's degree in engineering (preferably aeronautical engineering) or a closely related physical science with a minimum grade point average of 3.0 in the last 90 quarter u nits (60 semester units) attempted.

Applicants are required to submit satisfactory scores for the General (Aptitude) Test and Subject (Advanced) Test of the Graduate Record Examination in engineering.

An applicant who meets these standards but lacks prerequisite coursework may be admitted as a conditionally classified student and must make up any deficiencies before advancement to classified graduate standing.

Information pertaining to specific requirements for admission to graduate standing (classified or conditionally classified) may be obtained from the Graduate Coordinator, Department of Aeronautical Engineering.

Program of Study

Graduate students must file a formal study plan with their adviser, department, college and university graduate studies office by no later than the end of the quarter in which the 12th unit of approved courses is completed.

The formal program of study must include a minimum of 45 units (at least 24 of which must be at the 500 level).

A thesis or project is required as a culminating experience.

 

M.S. AERONAUTICAL ENGINEERING

Units

Required Courses

25

AERO 520 Theoretical Aerodynamics (3)

AERO 522 Boundary Layer Theory (3)

AERO 535 Advanced Aerospace Structural Analysis (3)

AERO 540 Elements of Rocket Propulsion (3)

AERO 550 Analysis and Design of Flight Control Systems (3)

AERO 590 Graduate Seminar (1)

AERO 599 Design Project (Thesis) (2) (2) (5)

Adviser approved electives

9

Advanced Mathematics/Analytical Methods for Engineers

11

MATH 501, MATH 502 Methods of Applied Mathematics I and II (4) (4)

AERO 515 Continuum Mechanics (3)

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45

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08/22/97