338-0547/01 – Ideal Fluid Dynamics (IFdyn)

Gurantor departmentDepartment of Hydromechanics and Hydraulic EquipmentCredits4
Subject guarantordoc. Ing. Sylva Drábková, Ph.D.Subject version guarantordoc. Ing. Sylva Drábková, Ph.D.
Study levelundergraduate or graduate
Study languageEnglish
Year of introduction2015/2016Year of cancellation
Intended for the facultiesFSIntended for study typesFollow-up Master, Bachelor, Master
Instruction secured by
LoginNameTuitorTeacher giving lectures
BLE02 doc. Ing. Tomáš Blejchař, Ph.D.
DRA10 doc. Ing. Sylva Drábková, Ph.D.
Extent of instruction for forms of study
Form of studyWay of compl.Extent
Full-time Credit and Examination 12+12

Subject aims expressed by acquired skills and competences

Students will be able to: • formulate the basic relations describing the behavior of ideal gases • explain the basic principles of steady and unsteady flow of an ideal fluid. Students will be able to: • analyze the problem of ideal fluid aerodynamics • choose a method for its solving • solve a given task • interprete and justify the obtained results

Teaching methods

Lectures
Tutorials

Summary

Compulsory literature:

ROY, Arnab&bookboon.com. A First Course on Aerodynamics. ISBN 978-87-7681-926-2. 100 p. Downloaded at http://bookboon.com/ ANDERSON J. D. Jr. Fundamentals of Aerodynamics. McGraw-Hill Higher Education. 2001. 912p. ISBN 0-07-237335-0

Recommended literature:

HOUGHTON E.L., CARPENTER, P. W. Aerodynamics for Engineering Students. Fifth Edition. Butterworth-Heinemann an imprint of Elsevier Science. 2003, 614 p., ISBN 0 7506 5111 3

Way of continuous check of knowledge in the course of semester

E-learning

Other requirements

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Prerequisities

Subject has no prerequisities.

Co-requisities

Subject has no co-requisities.

Subject syllabus:

Review of Navier-Stokes equations, perfect fluid approximation and consequences, Rankine-Hugoniot equations, Incompressible fluid dynamics: Review of airfoil profile study and determination of characteristics, Prandtl lifting line theory, lifting surface theory, Compressible fluid dynamics: o Subsonic flow and Prandtl-Glauert compressibility correction, o Slender body theory in subsonic flow, o Linearised two dimensional supersonic flow theory, shockwaves, - Applications in converging diverging nozzle.

Conditions for subject completion

Full-time form (validity from: 2015/2016 Winter semester)
Task nameType of taskMax. number of points
(act. for subtasks)
Min. number of points
Credit and Examination Credit and Examination 100 (100) 51
        Credit Credit 35  20
        Examination Examination 65  31
Mandatory attendence parzicipation:

Show history

Occurrence in study plans

Academic yearProgrammeField of studySpec.ZaměřeníFormStudy language Tut. centreYearWSType of duty

Occurrence in special blocks

Block nameAcademic yearForm of studyStudy language YearWSType of blockBlock owner
IPSA Paris 2021/2022 Full-time English Choice-compulsory 301 - Study and International Office stu. block
IPSA Paris 2020/2021 Full-time English Choice-compulsory 301 - Study and International Office stu. block
IPSA Paris 2019/2020 Full-time English Choice-compulsory 301 - Study and International Office stu. block
IPSA Paris 2018/2019 Full-time English Choice-compulsory 301 - Study and International Office stu. block
IPSA Paris 2017/2018 Full-time English Choice-compulsory 301 - Study and International Office stu. block
IPSA Paris 2016/2017 Full-time English Choice-compulsory 301 - Study and International Office stu. block
IPSA Paris 2015/2016 Full-time English Choice-compulsory 301 - Study and International Office stu. block