ME388 |
HELICOPTER AERONAUTICS |
2024 |
1 |
Civil and Mechanical Engineering |
3.0
(BS=0.0,
ET=3.0,
MA=0.0)
|
The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. The course analyzes the dynamic response of the rotor system and the performance aspects of the vehicle as a whole. This is followed by a design workshop, during which cadets complete the initial sizing of a helicopter to meet specific mission requirements. The course includes one flight lab in a helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company. |
28 @ 75 min (2.000 Att/wk) |
2 @ 120 min |
|
ME202 pre-requisite may be waived with validation exercise on structured programming and ME Program Director approval |
ME388 |
HELICOPTER AERONAUTICS |
2020 |
1 |
Civil and Mechanical Engineering |
3.0
(BS=0.0,
ET=3.0,
MA=0.0)
|
The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. The course analyzes the dynamic response of the rotor system and the performance aspects of the vehicle as a whole. This is followed by a design workshop, during which cadets complete the initial sizing of a helicopter to meet specific mission requirements. The course includes one flight lab in a helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company. |
28 @ 75 min (2.000 Att/wk) |
2 @ 120 min |
|
Graded design workshop, whirl-stand laboratory, and flight laboratory briefing. |
ME388 |
HELICOPTER AERONAUTICS |
2018 |
2 |
Civil and Mechanical Engineering |
3.0
(BS=0.0,
ET=3.0,
MA=0.0)
|
The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. The course analyzes the dynamic response of the rotor system and the performance aspects of the vehicle as a whole. This is followed by a design workshop, during which cadets complete the initial sizing of a helicopter to meet specific mission requirements. The course includes one flight lab in a helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company. |
38 @ 55 min (2.500 Att/wk) |
2 @ 120 min |
|
Graded design workshop, whirl-stand laboratory, and flight laboratory briefing. |
ME388 |
HELICOPTER AERONAUTICS |
2016 |
2 |
Civil and Mechanical Engineering |
3.0
(BS=0.0,
ET=3.0,
MA=0.0)
|
The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. The course analyzes the dynamic response of the rotor system and the performance aspects of the vehicle as a whole. This is followed by a design workshop, during which cadets complete the initial sizing of a helicopter to meet specific mission requirements. The course includes one flight lab in a helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company. |
38 @ 55 min (2.500 Att/wk) |
2 @ 120 min |
|
Graded design workshop, whirl-stand laboratory, and flight laboratory briefing. |
ME388 |
HELICOPTER AERONAUTICS |
2011 |
2 |
Civil and Mechanical Engineering |
3.0
(BS=0.0,
ET=3.0,
MA=0.0)
|
The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. The course analyzes the dynamic response of the rotor system and the performance aspects of the vehicle as a whole. This is followed by a design workshop, during which cadets complete the initial sizing of a helicopter to meet specific mission requirements. The course includes one flight lab in a helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company. |
38 @ 55 min (2.500 Att/wk) |
2 @ 120 min |
|
Graded design workshop, whirl-stand laboratory, and flight laboratory briefing. |
ME388 |
HELICOPTER AERONAUTICS |
2006 |
2 |
Civil and Mechanical Engineering |
3.0
(BS=0.0,
ET=3.0,
MA=0.0)
|
The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. The course analyzes the dynamic response of the rotor system and the performance aspects of the vehicle as a whole. This is followed by a design workshop, during which cadet groups complete the initial sizing of a helicopter to meet specific mission requirements. The course includes one flight lab in a UH-1 helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company. |
38 @ 55 min (2.500 Att/wk) |
2 @ 120 min |
|
Graded design workshop, whirl-stand laboratory, and flight laboratory briefing. |
ME388 |
HELICOPTER AERONAUTICS |
2004 |
1 |
Civil and Mechanical Engineering |
3.0
(BS=0.0,
ET=3.0,
MA=0.0)
|
The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. This is followed by a design workshop, during which cadet groups complete the initial sizing of a helicopter to meet specific mission requirements. The last third of the course analyzes the dynamic stability and response of both the rotor system and the vehicle. The course includes one flight lab in a UH-1 helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company. |
38 @ 55 min (2.500 Att/wk) |
2 @ 120 min |
|
Graded design workshop, whirl-stand laboratory, and flight laboratory reports. |
ME388 |
HELICOPTER AERONAUTICS |
1978 |
1 |
Civil and Mechanical Engineering |
3.0
(BS=0.0,
ET=3.0,
MA=0.0)
|
The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. This is followed by a design workshop, during which cadet groups complete the initial sizing of a helicopter to meet specific mission requirements. The last third of the course analyzes the dynamic stability and response of both the rotor system and the vehicle. The course includes one flight lab in a UH-1 helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company. |
38 @ 55 min (2.500 Att/wk) |
2 @ 120 min |
|
Graded design workshop, whirl-stand laboratory, and flight laboratory reports. |