Auxiliary Schedule of Classes

Schedule of Classes

Main Campus Class Schedule: spring 2021

CRN Course Section Cr Title Notes Days Times Place Instructor Cap
25751 AEE 1202 01 2 Aerospace Practicum
TR
M
0800-0915
1500-1550
501OEC 228
410GLE 107
Fleming 25/26
25752 AEE 1202 02 2 Aerospace Practicum
M
MR
1500-1550
1700-1815
410GLE 107
501OEC 228
Fleming 25/26
25753 AEE 1202 03 2 Aerospace Practicum
M
WF
1500-1550
1700-1815
410GLE 107
501OEC 228
Fleming 24/26
25754 AEE 1202 04 2 Aerospace Practicum
WF
M
0800-0915
1500-1550
501OEC 228
410GLE 107
Fleming 26/26
25755 AEE 1202 05 2 Aerospace Practicum
WF
M
0930-1045
1500-1550
501OEC 228
410GLE 107
Fleming 26/26
27381 AEE 1202 06 2 Aerospace Practicum
M
RF
1500-1550
1830-1945
410GLE 107
501OEC 228
Fleming 14/14
25774 AEE 3064 02 1 Fluid Mechanics Laboratory
T
0800-1030
538LAB 100
Subramanian 9/12
25775 AEE 3064 03 1 Fluid Mechanics Laboratory
T
1100-1330
538LAB 100
Subramanian 12/12
25776 AEE 3064 04 1 Fluid Mechanics Laboratory
T
1400-1630
538LAB 100
Subramanian 7/12
25777 AEE 3064 05 1 Fluid Mechanics Laboratory
W
0800-1030
538LAB 100
Subramanian 12/12
26456 AEE 3064 06 1 Fluid Mechanics Laboratory
W
1100-1330
538LAB 100
Subramanian 12/12
26570 AEE 3064 07 1 Fluid Mechanics Laboratory
W
1400-1630
538LAB 100
Subramanian 12/12
26768 AEE 3064 08 1 Fluid Mechanics Laboratory
R
0800-1030
538LAB 100
Subramanian 9/12
26769 AEE 3064 09 1 Fluid Mechanics Laboratory
R
1100-1330
538LAB 100
Subramanian 12/12
25778 AEE 3083 01 3 Mech of Materials
TR
1400-1515
623ATC 101
Rusovici 69/65
25779 AEE 3083 E1 3 Mech of Materials
TR
1700-1815
460SKU 110
Mirsayar 43/63
25782 AEE 3150 01 3 AE Comp Techniques
TR
1400-1515
410GLE 107
Archambault 106/95
25783 AEE 3161 01 3 Fluid Mechanics
MWF
1500-1550
623ATC 101
Zhang 62/70
25784 AEE 3162 01 3 Compressible Flow
TR
1530-1645
410GLE 107
Subramanian 37/40
26227 AEE 3162 E1 3 Compressible Flow
MW
1700-1815
410GLE 107
Harris 53/50
25789 AEE 3241 01 3 Aerodynamics & Flt Mech
TR
1100-1215
623ATC 101
Kirk 51/70
25790 AEE 3291 01 1 AE Junior Design
MW
1600-1650
410GLE 107
Demoret 51/49
26228 AEE 3291 02 1 AE Junior Design
MW
1600-1650
410GLE 107
Demoret 52/49
25791 AEE 4014 01 3 Control Systems
TR
1230-1345
410GLE 107
Tse 52/60
25801 AEE 4242 01 3 Aircraft Stab & Control
TBA 0/0
26770 AEE 4242 02 3 Aircraft Stab & Control
MWF
1300-1350
623ATC 101
Kish 76/70
25802 AEE 4261 01 3 Air-Breathing Engines
TR
0930-1045
410GLE 107
Archambault 73/85
25803 AEE 4281 01 3 Aerospace Structural Design
MW
1700-1815
420CRF 220
Fleming 26/48
26462 AEE 4281 02 3 Aerospace Structural Design
TR
1700-1815
410GLE 107
Fleming 70/70
25804 AEE 4284 01 1 Aero Eng Structures Lab
M
1100-1330
538LAB 102
Fleming 0/0
25805 AEE 4284 02 1 Aero Eng Structures Lab
T
1700-1930
538LAB 102
Fleming 0/0
25807 AEE 4284 04 1 Aero Eng Structures Lab
R
1700-1930
538LAB 102
Fleming 0/0
25808 AEE 4284 05 1 Aero Eng Structures Lab
R
1400-1630
538LAB 102
Fleming 9/12
26771 AEE 4284 06 1 Aero Eng Structures Lab
F
0800-1030
538LAB 102
Fleming 13/12
26772 AEE 4284 07 1 Aero Eng Structures Lab
F
1100-1330
538LAB 102
Fleming 11/12
25809 AEE 4292 01 3 Aero Eng Design 2
WF
1500-1650
410GLE 107
Demoret 49/49
26229 AEE 4292 02 3 Aero Eng Design 2
WF
1500-1650
410GLE 107
Demoret 30/49
27664 AEE 4400 01 3 Independent Study in AE
Wilde 1/1
25810 AEE 4806 01 3 Space Mission Engineering
TR
1530-1645
420CRF 112
Wilde 31/34
27930 AEE 5050 X1 3 Finite Element Fund
Fleming 1/0
25811 AEE 5060 E1 3 Applications in FEM
W
1700-1945
501OEC 128
Rusovici 15/25
27382 AEE 5130 E1 3 Viscous Flows
W
1000-1235
460SKU 219
Subramanian 5/12
27383 AEE 5360 E1 3 Hyp Airbreath Engns
TR
1830-1945
501OEC 137
Jahanbakhshi 7/24
26778 AEE 5590 01 3 Sel Top Contrls/Gdnce TOPIC: Space Mission Eng.
TR
1530-1645
420CRF 112
Wilde 7/6
27384 AEE 5802 E1 3 Multivar Feedback Control
TR
1700-1815
460SKU 116
Bronson 4/24
27961 AEE 5899 09 0-2 Final Semester Thesis
Rusovici 1/0
25826 AEE 5900 01 0 Aerospace Eng Seminar
F
1600-1650
501OEC 118
Fleming 10/56
25827 AEE 5999 01 3-6 Thesis
Archambault 1/5
25828 AEE 5999 02 3-6 Thesis
Demoret 0/5
25829 AEE 5999 03 3-6 Thesis
Fleming 4/5