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| CRN | Course | Section | Credits | Title | Notes | Days | Times | Place | Instructor | Enrolled/Limit |
|---|---|---|---|---|---|---|---|---|---|---|
| 84526 | AEE 1201 | 01 | 1 |
Intro to Aerospace Engineering
Provides a broad overview of the aerospace engineering profession through class meetings involving formal lectures and presentations, and site/laboratory visits. Introduces the concept of aerospace design as a precursor to a competitive freshman design project to be implemented in AEE 1202.
|
F |
1400-1450 |
501OEC 118 |
Kirk | 38/45 | |
| 85121 | AEE 1201 | 02 | 1 |
Intro to Aerospace Engineering
Provides a broad overview of the aerospace engineering profession through class meetings involving formal lectures and presentations, and site/laboratory visits. Introduces the concept of aerospace design as a precursor to a competitive freshman design project to be implemented in AEE 1202.
|
F |
1400-1450 |
501OEC 118 |
Kirk | 38/45 | |
| 85148 | AEE 1201 | 03 | 1 |
Intro to Aerospace Engineering
Provides a broad overview of the aerospace engineering profession through class meetings involving formal lectures and presentations, and site/laboratory visits. Introduces the concept of aerospace design as a precursor to a competitive freshman design project to be implemented in AEE 1202.
|
F |
1400-1450 |
501OEC 118 |
Kirk | 39/45 | |
| 85149 | AEE 1201 | 04 | 1 |
Intro to Aerospace Engineering
Provides a broad overview of the aerospace engineering profession through class meetings involving formal lectures and presentations, and site/laboratory visits. Introduces the concept of aerospace design as a precursor to a competitive freshman design project to be implemented in AEE 1202.
|
F |
1400-1450 |
501OEC 118 |
Kirk | 39/45 | |
| 84527 | AEE 2201 | 01 | 2 |
Aerospace Fundamentals
Introduces the theory and analysis of structures, aerodynamics, propulsion and control. Presents the theoretical advances and continuing developments from a historical perspective by stressing the roles and contributions of pioneers. (Prerequisites: AEE 1202, MAE 1202, MTH 1002, MTH 1020, PHY 1001)
|
TR |
1400-1450 |
500OLS 130 |
Kirk | 45/49 | |
| 84528 | AEE 2201 | 02 | 2 |
Aerospace Fundamentals
Introduces the theory and analysis of structures, aerodynamics, propulsion and control. Presents the theoretical advances and continuing developments from a historical perspective by stressing the roles and contributions of pioneers. (Prerequisites: AEE 1202, MAE 1202, MTH 1002, MTH 1020, PHY 1001)
|
TR |
1200-1250 |
500OLS 130 |
Wilde | 41/49 | |
| 84574 | AEE 3064 | 01 | 1 |
Fluid Mechanics Laboratory
Provides a working familiarity with the physical principles, measurement and flow visualization techniques in fluid mechanics. (Prerequisites: AEE 3161, AEE 3161, PHY 2092)
|
T |
0800-1045 |
427FRU 119 |
Subramanian | 15/15 | |
| 84575 | AEE 3064 | 02 | 1 |
Fluid Mechanics Laboratory
Provides a working familiarity with the physical principles, measurement and flow visualization techniques in fluid mechanics. (Prerequisites: AEE 3161, AEE 3161, PHY 2092)
|
F |
1100-1345 |
427FRU 119 |
Subramanian | 13/15 | |
| 84576 | AEE 3064 | 03 | 1 |
Fluid Mechanics Laboratory
Provides a working familiarity with the physical principles, measurement and flow visualization techniques in fluid mechanics. (Prerequisites: AEE 3161, AEE 3161, PHY 2092)
|
T |
1400-1645 |
427FRU 119 |
Subramanian | 6/15 | |
| 84577 | AEE 3064 | 04 | 1 |
Fluid Mechanics Laboratory
Provides a working familiarity with the physical principles, measurement and flow visualization techniques in fluid mechanics. (Prerequisites: AEE 3161, AEE 3161, PHY 2092)
|
M |
1400-1645 |
427FRU 119 |
Subramanian | 12/15 | |
| 84578 | AEE 3064 | 05 | 1 |
Fluid Mechanics Laboratory
Provides a working familiarity with the physical principles, measurement and flow visualization techniques in fluid mechanics. (Prerequisites: AEE 3161, AEE 3161, PHY 2092)
|
R |
1100-1345 |
427FRU 119 |
Subramanian | 12/15 | |
| 84579 | AEE 3064 | 06 | 1 |
Fluid Mechanics Laboratory
Provides a working familiarity with the physical principles, measurement and flow visualization techniques in fluid mechanics. (Prerequisites: AEE 3161, AEE 3161, PHY 2092)
|
M |
0800-1045 |
427FRU 119 |
Subramanian | 14/15 | |
| 84580 | AEE 3064 | 07 | 1 |
Fluid Mechanics Laboratory
Provides a working familiarity with the physical principles, measurement and flow visualization techniques in fluid mechanics. (Prerequisites: AEE 3161, AEE 3161, PHY 2092)
|
W |
1100-1345 |
427FRU 119 |
Subramanian | 15/15 | |
| 84581 | AEE 3064 | 08 | 1 |
Fluid Mechanics Laboratory
Provides a working familiarity with the physical principles, measurement and flow visualization techniques in fluid mechanics. (Prerequisites: AEE 3161, AEE 3161, PHY 2092)
|
T |
1100-1345 |
427FRU 119 |
Subramanian | 7/15 | |
| 84582 | AEE 3083 | 01 | 3 |
Mech of Materials
Covers stress and strain; mechanical properties of materials; Hooke's law; axial, torsion, pure-bending and transverse loading of members; transformations of stress and strain; failure criteria; strain measurements; thin-walled pressure vessels; design for strength; energy methods; design for impact; and column buckling and stability. (Prerequisites: MAE 2081, MEE 2081)
|
TR |
1530-1645 |
500OLS 129 |
Fleming | 41/44 | |
| 84583 | AEE 3083 | 02 | 3 |
Mech of Materials
Covers stress and strain; mechanical properties of materials; Hooke's law; axial, torsion, pure-bending and transverse loading of members; transformations of stress and strain; failure criteria; strain measurements; thin-walled pressure vessels; design for strength; energy methods; design for impact; and column buckling and stability. (Prerequisites: MAE 2081, MEE 2081)
|
TR TR |
1530-1645 1530-1645 |
502OPS 140 420CRF 230 |
Di Pasquale | 27/44 | |
| 84584 | AEE 3083 | 03 | 3 |
Mech of Materials
Covers stress and strain; mechanical properties of materials; Hooke's law; axial, torsion, pure-bending and transverse loading of members; transformations of stress and strain; failure criteria; strain measurements; thin-walled pressure vessels; design for strength; energy methods; design for impact; and column buckling and stability. (Prerequisites: MAE 2081, MEE 2081)
|
TR |
0930-1045 |
460SKU 116 |
Di Pasquale | 42/44 | |
| 84585 | AEE 3161 | 01 | 3 |
Fluid Mechanics
Introduces fluid variables; fluid statics; flow kinematics; equations of mass, momentum and energy conservation in both integral and differential formulations; similitude and dimensional analysis; the stress tensor; inviscid and viscous flows; flow in pipes; and laminar and turbulent flow. (Prerequisites: MAE 2082, MEE 2082, PHY 3011, MTH 2001, MTH 2010, MTH 2201, MTH 3200, MAE 2082, MEE 2082, PHY 3011, MTH 2001, MTH 2010, MTH 2201, MTH 3200)
|
MWF |
1400-1450 |
460SKU 102 |
Sepri | 36/44 | |
| 84586 | AEE 3161 | 02 | 3 |
Fluid Mechanics
Introduces fluid variables; fluid statics; flow kinematics; equations of mass, momentum and energy conservation in both integral and differential formulations; similitude and dimensional analysis; the stress tensor; inviscid and viscous flows; flow in pipes; and laminar and turbulent flow. (Prerequisites: MAE 2082, MEE 2082, PHY 3011, MTH 2001, MTH 2010, MTH 2201, MTH 3200, MAE 2082, MEE 2082, PHY 3011, MTH 2001, MTH 2010, MTH 2201, MTH 3200)
|
TR |
1100-1215 |
428EVL 133 |
Zhang | 48/50 | |
| 84587 | AEE 3161 | 03 | 3 |
Fluid Mechanics
Introduces fluid variables; fluid statics; flow kinematics; equations of mass, momentum and energy conservation in both integral and differential formulations; similitude and dimensional analysis; the stress tensor; inviscid and viscous flows; flow in pipes; and laminar and turbulent flow. (Prerequisites: MAE 2082, MEE 2082, PHY 3011, MTH 2001, MTH 2010, MTH 2201, MTH 3200, MAE 2082, MEE 2082, PHY 3011, MTH 2001, MTH 2010, MTH 2201, MTH 3200)
|
TR |
1400-1515 |
420CRF 220 |
Zhang | 49/50 | |
| 84568 | AEE 3260 | 01 | 3 |
Experimental Aerodynamics
Offers theory and practice in wind tunnel test techniques, measurements of lift and drag by force balance, pressure distributions and wake surveys, LDA, thermal anemometry, and computer-based data acquisition and reduction using LabView and uncertainty analysis. (Prerequisites: AEE 3161, MAE 3161, MAE 3064, AEE 3064)
|
F MW |
1100-1345 1400-1450 |
538LAB 100 501OEC 118 |
Kish | 11/12 | |
| 84569 | AEE 3260 | 02 | 3 |
Experimental Aerodynamics
Offers theory and practice in wind tunnel test techniques, measurements of lift and drag by force balance, pressure distributions and wake surveys, LDA, thermal anemometry, and computer-based data acquisition and reduction using LabView and uncertainty analysis. (Prerequisites: AEE 3161, MAE 3161, MAE 3064, AEE 3064)
|
T MW |
1100-1345 1400-1450 |
538LAB 100 501OEC 118 |
Kish | 12/12 | |
| 84570 | AEE 3260 | 03 | 3 |
Experimental Aerodynamics
Offers theory and practice in wind tunnel test techniques, measurements of lift and drag by force balance, pressure distributions and wake surveys, LDA, thermal anemometry, and computer-based data acquisition and reduction using LabView and uncertainty analysis. (Prerequisites: AEE 3161, MAE 3161, MAE 3064, AEE 3064)
|
M MW |
1100-1345 1400-1450 |
538LAB 100 501OEC 118 |
Kish | 13/12 | |
| 84571 | AEE 3260 | 04 | 3 |
Experimental Aerodynamics
Offers theory and practice in wind tunnel test techniques, measurements of lift and drag by force balance, pressure distributions and wake surveys, LDA, thermal anemometry, and computer-based data acquisition and reduction using LabView and uncertainty analysis. (Prerequisites: AEE 3161, MAE 3161, MAE 3064, AEE 3064)
|
MW F |
1400-1450 1400-1645 |
501OEC 118 538LAB 100 |
Kish | 12/12 | |
| 84572 | AEE 3260 | 05 | 3 |
Experimental Aerodynamics
Offers theory and practice in wind tunnel test techniques, measurements of lift and drag by force balance, pressure distributions and wake surveys, LDA, thermal anemometry, and computer-based data acquisition and reduction using LabView and uncertainty analysis. (Prerequisites: AEE 3161, MAE 3161, MAE 3064, AEE 3064)
|
R MW |
1100-1345 1400-1450 |
538LAB 100 501OEC 118 |
Kish | 13/12 | |
| 84573 | AEE 3260 | 06 | 3 |
Experimental Aerodynamics
Offers theory and practice in wind tunnel test techniques, measurements of lift and drag by force balance, pressure distributions and wake surveys, LDA, thermal anemometry, and computer-based data acquisition and reduction using LabView and uncertainty analysis. (Prerequisites: AEE 3161, MAE 3161, MAE 3064, AEE 3064)
|
F MW |
0800-1045 1400-1450 |
538LAB 100 501OEC 118 |
Kish | 12/12 | |
| 84567 | AEE 4014 | 01 | 3 |
Control Systems
Stresses both classical and modern control methodologies. Includes frequency and time-domain representation of linear systems, stability analysis and design techniques. (Prerequisites: MTH 2201, MTH 3200)
|
TR |
1530-1645 |
460SKU 110 |
Go | 68/75 | |
| 84556 | AEE 4262 | 01 | 3 |
Rockets & Mission Analysis
Deals with performance analysis of rockets. Emphasizes chemical rocket propulsion, thrust and specific impulse, mission requirements and rocket staging; solid- and liquid-propellant rockets and propellants; and orbital mechanics and mission analyses. (Prerequisites: AEE 3162, MAE 3162)
|
TR |
0930-1045 |
428EVL 133 |
Archambault | 71/75 | |
| 84558 | AEE 4263 | 01 | 3 |
Space Flight Mechanics
Provides understanding of the motion of celestial objects and spacecraft under gravity. Includes analysis of the two-body and restricted three-body problems and orbital transfer using impulsive forces. Also includes designing interplanetary spacecraft trajectories for given specifications. Uses MATLAB(r) for numerical analyses and dynamic simulation. (Prerequisites: MAE 2082, MEE 2082, MTH 2201, MTH 3200)
|
MWF |
1100-1150 |
420CRF 401 |
Kaplinger | 32/50 | |
| 84557 | AEE 4263 | E1 | 3 |
Space Flight Mechanics
Provides understanding of the motion of celestial objects and spacecraft under gravity. Includes analysis of the two-body and restricted three-body problems and orbital transfer using impulsive forces. Also includes designing interplanetary spacecraft trajectories for given specifications. Uses MATLAB(r) for numerical analyses and dynamic simulation. (Prerequisites: MAE 2082, MEE 2082, MTH 2201, MTH 3200)
|
TR |
1700-1815 |
500OLS 129 |
Wilde | 49/50 | |
| 84559 | AEE 4291 | 01 | 3 |
Aero Eng Design 1
Includes design of an aircraft, spacecraft or component to meet desired needs. Students are given a simulated request for proposals including a measure of merit and a set of specifications that a satisfactory design must meet. Teams work under faculty supervision to develop a design to best meet these requirements. Students present their designs in written reports at the end of each semester. Introduces some of the ethical and legal issues engineers must face. (Requirement: Senior standing.) (Q) (Prerequisites: AEE 3291, MAE 3291)
|
MW |
1500-1650 |
420CRF 112 |
Demoret | 47/49 | |
| 84729 | AEE 4291 | 02 | 3 |
Aero Eng Design 1
Includes design of an aircraft, spacecraft or component to meet desired needs. Students are given a simulated request for proposals including a measure of merit and a set of specifications that a satisfactory design must meet. Teams work under faculty supervision to develop a design to best meet these requirements. Students present their designs in written reports at the end of each semester. Introduces some of the ethical and legal issues engineers must face. (Requirement: Senior standing.) (Q) (Prerequisites: AEE 3291, MAE 3291)
|
MW |
1500-1650 |
420CRF 112 |
Demoret | 19/49 | |
| 84560 | AEE 5130 | E1 | 3 |
Viscous Flows
Includes theory of Navier-Stokes equations; exact solutions for steady and unsteady plane, duct, jet and stagnation point flows; Stokes and Oseen approximations; the Prandtl concept of the boundary layer and similarity solutions Blasius, Hiemenz, Faulkner and Skan, Hartree, etc.; and approximate solutions for nonsimilar boundary layers.
|
TR |
1830-1945 |
420CRF 526 |
Subramanian | 12/24 | |
| 84561 | AEE 5150 | E1 | 3 |
Computnl Fluid Dynamics
Includes elliptic, parabolic and hyperbolic PDEs; finite-difference formulations; explicit and implicit methods and stability analysis; operator splitting and multi-step methods; boundary conditions; grid generation techniques; and applications involving Euler boundary layer and full Navier-Stokes equations. (Requirement: Background knowledge in Fortran, C/C++ or other programming language (other than MATLAB or similar), and partial differential equations.)
|
TR |
1700-1815 |
420CRF 212 |
Archambault | 9/25 | |
| 84562 | AEE 5470 | E1 | 3 |
Princ of Composite Matls
Covers particulate and fiber composites; form, properties and processing of constituent materials; manufacture of composites, interaction of constituents, micro- and macro-mechanics and design of composite materials; stress-strain tensors and their transformation; laminate theory of orthotropic materials; and strength properties.
|
MW |
1700-1815 |
420CRF 527 |
Fleming | 8/25 | |
| 84563 | AEE 5480 | E1 | 3 |
Struct Dynamics
Applies the principles of dynamics to structural analysis, analysis of continuous media and discretized models, free vibration and forced response of structures, modal analysis, energy methods and approximate methods, and applications in structural design and experimentation.
|
T |
1700-1945 |
501OEC 137 |
Rusovici | 13/25 | |
| 85075 | AEE 5590 | 01 | 3 |
Sel Top Contrls/Gdnce
Addresses selected topics reflecting the current interests of the faculty and visiting scholars.
|
TR |
1600-1715 |
402QAD 110 |
Kaplinger | 3/6 | |
| 84566 | AEE 5802 | E1 | 3 |
Multivar Feedback Control
Includes modern analysis and control design approaches for linear multivariable systems. Includes modeling of dynamic systems, concept of controllability and observability, eigenstructure assignment technique, singular value decomposition, stability robustness and optimum control methods. (Requirement: Background knowledge of control systems.)
|
MW MW |
1700-1815 1700-1815 |
501OEC 137 420CRF 212 |
Go | 15/30 | |
| 85005 | AEE 5899 | 01 | 0-2 |
Final Semester Thesis
Variable registration for thesis completion after satisfaction of minimum registration requirements. (Requirements: Accepted petition to graduate and approval by Office of Graduate Programs.)
|
Archambault | 0/1 | ||||
| 85127 | AEE 5899 | 08 | 0-2 |
Final Semester Thesis
Variable registration for thesis completion after satisfaction of minimum registration requirements. (Requirements: Accepted petition to graduate and approval by Office of Graduate Programs.)
|
Kish | 1/0 | ||||
| 84555 | AEE 5900 | 01 | 0 |
Aerospace Eng Seminar
Presents current research by university faculty, visiting speakers and graduate students. Required of all full-time aerospace engineering students.
|
F |
1600-1650 |
428EVL 133 |
Fleming | 16/90 | |
| 85073 | AEE 5997 | 01 | 1-3 |
Independent Study
Individual study under the direction of a member of the aerospace engineering graduate faculty.
|
TOPIC: Analysis of Bonded Joints |
TR |
1530-1645 |
Fleming | 2/2 | |
| 84529 | AEE 5999 | 01 | 3-6 |
Thesis
Individual work under the direction of a member of the aerospace engineering graduate faculty on a selected topic.
|
Archambault | 2/5 | ||||
| 84530 | AEE 5999 | 02 | 3-6 |
Thesis
Individual work under the direction of a member of the aerospace engineering graduate faculty on a selected topic.
|
Demoret | 0/5 | ||||
| 84531 | AEE 5999 | 03 | 3-6 |
Thesis
Individual work under the direction of a member of the aerospace engineering graduate faculty on a selected topic.
|
Fleming | 0/5 | ||||
| 84532 | AEE 5999 | 04 | 3-6 |
Thesis
Individual work under the direction of a member of the aerospace engineering graduate faculty on a selected topic.
|
Go | 1/5 | ||||
| 84533 | AEE 5999 | 05 | 3-6 |
Thesis
Individual work under the direction of a member of the aerospace engineering graduate faculty on a selected topic.
|
Kaplinger | 0/5 | ||||
| 84534 | AEE 5999 | 06 | 3-6 |
Thesis
Individual work under the direction of a member of the aerospace engineering graduate faculty on a selected topic.
|
Kimberlin | 0/5 | ||||
| 84535 | AEE 5999 | 07 | 3-6 |
Thesis
Individual work under the direction of a member of the aerospace engineering graduate faculty on a selected topic.
|
Kirk | 3/5 | ||||
| 84536 | AEE 5999 | 08 | 3-6 |
Thesis
Individual work under the direction of a member of the aerospace engineering graduate faculty on a selected topic.
|
Kish | 3/5 |
