Educational guide

IDENTIFYING DATA

2024_25

Subject

ADVANCED FLUID MECHANICS.

Code

00713008

Study programme

0713 - MASTER UNIV. EN INGENIERIA AERONAUTICA

Descriptors

Credit.

Type

Year

Period

4.5

Compulsory

First

Second

Language

Castellano

Ingles

Prerequisites

Department

QUIMICA Y FISICA APLICADAS

Coordinador

GARCÍA ORTEGA , EDUARDO

E-mail

egaror@unileon.es
jlsang@unileon.es

Lecturers

GARCÍA ORTEGA , EDUARDO

SÁNCHEZ GÓMEZ , JOSÉ LUIS

Web

http://

General description

Tribunales de Revisión

Tribunal titular
Cargo	Departamento	Profesor
Presidente	QUIMICA Y FISICA APLICADAS	LOPEZ CAMPANO , LAURA
Secretario	QUIMICA Y FISICA APLICADAS	MARCOS MENENDEZ , JOSE LUIS
Vocal	QUIMICA Y FISICA APLICADAS	MERINO SUANCES , ANDRES

Tribunal suplente
Cargo	Departamento	Profesor
Presidente	QUIMICA Y FISICA APLICADAS	CEPEDA RIAÑO , JESUS RAMIRO
Secretario	QUIMICA Y FISICA APLICADAS	BURDALO SALCEDO , GABRIEL
Vocal	QUIMICA Y FISICA APLICADAS	ZORITA CALVO , MIGUEL

Competencies

Type A	Code	Competences Specific
	A13177
	A13178
	A13179
	A13183
	A13189
	A13190
	A13204
	A13216
Type B	Code	Competences Transversal
	B3012
	B3013
	B3039
	B3048
	B3050
	B3051
Type C	Code	Competences Nuclear
	C1
	C2
	C3
	C4

Learning aims

	Competences
That the student understands the behavior of compressible flows at subsonic, sonic, and supersonic velocities.	A13204	B3012 B3013 B3039	C1 C2 C3
That the student knows and applies the responses of bodies in motion within viscous fluids	A13178 A13179 A13204 A13216		C1 C2 C3 C4
That the student understands the principles of flight from the perspective of fluid mechanics	A13177 A13204	B3048 B3050 B3051	C1 C2 C3 C4
	A13183 A13189 A13190

Contents

Topic	Sub-topic
Part I: INVISCID COMPRESSIBLE FLOW	Chapter 1: PRELIMINARY ASPECTS. Thermodynamics; compressibility;governing equations; definition of total (stagnation) conditions. Chapter 2: NORMAL SHOCK WAVES. Equations and speed of sound; special forms of the energy; compressible flow threshold; normal shock-wave properties; measurement of velocity in a compressible flow. Chapter 3: COMPRESSIBLE FLOW THROUGH NOZZLES, DIFFUSERS AND WIND TUNNELS. Governing equations for quasi-one-dimensional flow; nozzle flows; diffusers; supersonic wind tunnels. Chapter 4: SUBSONIC COMPRESSIBLE FLOW OVER AIRFOILS: LINEAR THEORY. Velocity potential equation; linearized velocity potential equation; Prantdl-Glauert compressibility correction. Chapter 5: LINEARIZED SUPERSONIC FLOW AND HYPERSONIC FLOW. Linearized supersonic pressure coefficient; application; qualitative aspects of hypersonic flow.
Part II: VISCOUS FLOW	Chapter 1 (6): FUNDAMENTAL PRINCIPLES AND EQUATIONS OF VISCOUS FLOW. Atmospheric boundary layer; laminar and turbulent flow; Qualitative aspects; viscosity and thermal conduction; the Navier-Stokes equations; energy equation; solutions of viscous flows; Couette flow. Chapter 2 (7): INTRODUCTION TO BOUNDARY LAYERS. Boundary-layer properties; the boundary-layer equations. Chapter 3 (8): LAMINAR AND TURBULENT BOUNDARY LAYERS. Incompressible and compressible flow over a flat plate; turbulent flow on a flat plate.

Planning

Methodologies :: Tests
	Class hours	Hours outside the classroom	Total hours
Seminars	3	3	6

Problem solving, classroom exercises	5	5.5	10.5
Field work/trips	6	9	15
Tutorship of group	1	0	1
Assignments	2.5	12.5	15

Lecture	25	37.5	62.5

Extended-answer tests	2.5	0	2.5

(*)The information in the planning table is for guidance only and does not take into account the heterogeneity of the students.

Methodologies

Methodologies ::

	Description
Seminars
Problem solving, classroom exercises
Field work/trips
Tutorship of group
Assignments
Lecture

Personalized attention

Description

Assessment

	Description	Qualification
Lecture	Exam with content covered in the course, including both theoretical and practical aspects. In this part, students must obtain at least 2.5 points out of 6 to be eligible for compensatio	6
Assignments	Mandatory attendance to practical sessions. Submission and presentation of the proposed group assignments/projects. In case of non-attendance to the practical sessions, the student will receive a grade of 0 for this part in the first assessment period.	3
Others	Confirmed attendance to 90% of classes	1

Other comments and second call
Assessment in the first assessment period: There will be a theoretical/practical written exam with a maximum score of 6 points, to which the score obtained in the assignment (up to a maximum of 3 points) will be added. An additional point can be obtained by confirming attendance to class of 90% or higher. Assessment in the second assessment period: It will be evaluated through a theoretical/practical written exam with a maximum score of 7 points, to which the score obtained in the assignment/practical project (up to a maximum of 3 points) will be added. In order to prevent plagiarism and ensure equal opportunities for all students, the possession and use of mobile and/or electronic devices, notes, books, folders, or other unauthorized materials during assessments will not be allowed. This is in accordance with the guidelines established by the University regarding plagiarism, copying, or fraud in exams or assessments. Simply possessing such devices during assessments will result in immediate removal from the exam, expulsion, and a failing grade.

Sources of information

Access to Recommended Bibliography in the Catalog ULE

Basic	John Anderson Jr. , Fundamentals of aerodynamics, MacGraw Hill, Frank M. White, Mecánica de Fluidos, McGraw Hill, Irving H. Shames, Mecánica de fluidos, MacGraw Hill,

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