Helicopter Engineering

HIRAMOTO, Takashi
  Elective  2 credits
【Master's program・2nd semester】
19-3-1023-3035

1.
Outline
In this course, students will design a helicopter of the scale that they chose themselves according to typical conceptual design methods that will be shown in the lectures. Students will understand numerically the aerodynamics of the rotor and the flight dynamics of the helicopter through the design.
2.
Objectives
The goal of this course is to understand the flight mechanism and aerodynamics of the helicopter through the conceptual design of the original helicopter according to basic process. In addition, the lectures address problems that should be settled by the helicopter design and aim to understand flight properties and performances.
3.
Grading Policy
Results will be evaluated by reports with own design procedure and discussion in the lecture.
4.
Textbook and Reference
Texts and some materials will be distributed.
5.
Requirements (Assignments)
It is desirable for students to have studied "Introduction to Helicopter Engineering" in the undergraduate course. Furthermore, “Fundamental Design Technology of an Airplane” and “Airplane Dynamics” will also be needed. In the lectures, the supplemental explanation shall be given with the presentation materials depending on the understanding level of participants. However, a preparation learning with using the reference books introduced in the class is recommended.
6.
Note
Students will design a helicopter based on what they learn in lectures. They will give presentations about the design progress status when appropriate and discuss their results.
Reference book: W.J. Wagtendonk, “Principles Helicopter Flight”, Aviation Supplies & Academics, Inc.
7.
Schedule
1. Design process – Development process of aircraft
2. Helicopter design – Setting of helicopter scale
3. Main rotor design, part 1 – Momentum theory and wing element theory
4. Main rotor design, part 2 – Setting of main rotor sizing
5. Assumption of power, part 1 – About power of helicopter
6. Assumption of power, part 2 – Required power
7. Landing gear – Construction and choice of landing gear
8. Specifications – Result and confirmation
9. Tail rotor design – Tail rotor sizing
10. Refinement of power estimation, part 1 – Weight evaluation
11. Refinement of power estimation, part 2 – Confirmation of concept
12. Choice of engine
13. Confirmation of basic performance
14. Three view drawing
15. Presentation of design
1.
Outline
In this course, students will design a helicopter of the scale that they chose themselves according to typical conceptual design methods that will be shown in the lectures. Students will understand numerically the aerodynamics of the rotor and the flight dynamics of the helicopter through the design.
2.
Objectives
The goal of this course is to understand the flight mechanism and aerodynamics of the helicopter through the conceptual design of the original helicopter according to basic process. In addition, the lectures address problems that should be settled by the helicopter design and aim to understand flight properties and performances.
3.
Grading Policy
Results will be evaluated by reports with own design procedure and discussion in the lecture.
4.
Textbook and Reference
Texts and some materials will be distributed.
5.
Requirements (Assignments)
It is desirable for students to have studied "Introduction to Helicopter Engineering" in the undergraduate course. Furthermore, “Fundamental Design Technology of an Airplane” and “Airplane Dynamics” will also be needed. In the lectures, the supplemental explanation shall be given with the presentation materials depending on the understanding level of participants. However, a preparation learning with using the reference books introduced in the class is recommended.
6.
Note
Students will design a helicopter based on what they learn in lectures. They will give presentations about the design progress status when appropriate and discuss their results.
Reference book: W.J. Wagtendonk, “Principles Helicopter Flight”, Aviation Supplies & Academics, Inc.
7.
Schedule
1. Design process – Development process of aircraft
2. Helicopter design – Setting of helicopter scale
3. Main rotor design, part 1 – Momentum theory and wing element theory
4. Main rotor design, part 2 – Setting of main rotor sizing
5. Assumption of power, part 1 – About power of helicopter
6. Assumption of power, part 2 – Required power
7. Landing gear – Construction and choice of landing gear
8. Specifications – Result and confirmation
9. Tail rotor design – Tail rotor sizing
10. Refinement of power estimation, part 1 – Weight evaluation
11. Refinement of power estimation, part 2 – Confirmation of concept
12. Choice of engine
13. Confirmation of basic performance
14. Three view drawing
15. Presentation of design