| Code |
10381
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| Year |
4
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| Semester |
S1
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| ECTS Credits |
6
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| Workload |
TP(60H)
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| Scientific area |
Aeronautics and Astronautics
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Entry requirements |
No prerequisites
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Mode of delivery |
This unit classes are theoretical-practical. Theoretical foundations are presented initially and after the practical applications, with examples of calculation. Presentations are made using a computer and video projector. Calculations are made at the white board. All documentation is provided to the students on an e-learning platform.
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Work placements |
There is no work placement.
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Learning outcomes |
Knowledge of fundamental concepts related to high speed flight.
Capacity analysis and design in steady one-dimensional flow adiabatic and isentropic.
Capacity analysis and design in one-dimensional isentropic flow with area change.
Capacity of analysis of normal shock waves.
Ability to design convergent-divergent nozzles.
Capacity of analysis and design in one-dimensional compressible flow with friction.
Capacity of analysis and design in one-dimensional compressible flow with heat transfer.
Capacity of analysis and design in two-dimensional supersonic flow.
Capacity of analysis and design in transonic flow.
Capacity of analysis and design in hypersonic flow.
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Syllabus |
1. Fundamental concepts associated with gas dynamics. Mach number. Perfect gases.
2. Steady one-dimensional adiabatic and isentropic flow. Relations as function of Mach number. Critical values at the sonic point. Simplified expressions for air.
3. One-dimensional isentropic flow with area change. Relations for ideal gases. Choking by area change.
4. Normal shock waves. Relations using the Mach number. Non-stationary shock waves. Oblique shock waves.
5. Nozzles and diffusers.
6. One-dimensional compressible flow with friction. Adiabatic flow. Choking due to friction. Isothermal flow with friction.
7. One-dimensional compressible flow with heat transfer. Choking due to heating.
8. Supersonic two-dimensional flow.
9. Transonic flow.
10. Hypersonic flow.
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Main Bibliography |
Zucker, R.; Biblarz, O,; Fundamentals of Gas Dynamics, John Wiley & Sons
Anderson, J. D. Jr, Hypersonic and High Temperature Gas Dynamics, McGraw Hill Book Co.
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Teaching Methodologies and Assessment Criteria |
The classes of this course unit are theoretical-practical. The theoretical foundations are presented initially and then the practical applications, with examples of calculation. Presentations are made using a computer and video projector. Calculations of the practical component are done in the table. All documentation is provided to students on an e-learning platform.
Periodic assessment is based on an exam.
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Language |
Portuguese. Tutorial support is available in English.
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