Aerodynamics 3
TeachersKAWAMURA, Masaaki
Grade, SemesterYear 3 1st semest [Department of Aerospace Engineering, Faculty of Science and Engineering]
CategorySpecial Subjects
Elective, CreditsElective 2credit
 Syllabus Number2A311

Course Description

Students learn following contents in this class.
1. Compressible fluid : change of density, sound velocity and Mach number, subsonic flow and supersonic flow, thermodynamics
2. One-dimensional flow : basic equation, sound wave, energy equation of adiabatic flow, isentropic flow
3. Normal shock wave : Rankine-Hugoniot equation
4. Oblique shock wave : shock angle
Students can acquire knowledge about DP2 in this class.

Course Objectives

Goal of this class is that students comprehend basic phenomenon and basic lows about compressible flow which influences high speed airplane or inner flow of jet engine etc. Moreover, student can study shock wave caused by supersonic flow.

Grading Policy

Attendance more than two thirds, midterm exam (40%) and term end exam (60%).
The students will get simple explanations after these exams.

Textbook and Reference

KindTitleAuthorPublisher
Textbook
References ISBN978-4274069697
ReferencesISBN978-4990748333
ReferencesISBN978-4621089705
References ISBN978-4339046533

Requirements(Assignments)

Review incompressible fluid dynamics, thermodynamics, elementary dynamics, infinitesimal calculus and differential equation thoroughly.
Read the text within the contents of the next lecture and write in a notebook for preparation in order to comprehend meaning of technical terms (1.5 hours).
After the lecture will be ended, review the notebook teacher explains in the class (1.5 hours).

Note

Schedule

1Introduction of compressible flow and thermodynamics (1) : compressible flow
2Introduction of compressible flow and thermodynamics (2) : sound velocity and Mach number
3Introduction of compressible flow and thermodynamics (3) : equation of state
4Introduction of compressible flow and thermodynamics (4) : first low of thermodynamics
5Introduction of compressible flow and thermodynamics (5) : entropy and enthalpy
6One-dimensional flow (1) : basic equation
7One-dimensional flow (2) : sound wave, sound velocity
8Summary of the former part, Midterm exam
9One-dimensional flow (3) : isentropic flow
10One-dimensional flow (4) : nozzle theory
11Shock theory (1) : normal shock wave 1
12Shock theory (2) : Rankine-Hugoniot equation
13Shock theory (3) : normal shock wave 2
14Shock theory (4) : oblique shock wave
15Summary, Term end exam