Educational guide
IDENTIFYING DATA							2023_24
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
	A13204	B3012 B3013 B3039	C1 C2 C3
	A13178 A13179 A13204 A13216		C1 C2 C3 C4
	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		7
Assignments		3
Other comments and second call

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,
Complementary

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