Anna University Syllabus - Anna University ME Syllabus
AO7011 HYPERSONIC AERODYNAMICS Syllabus | Anna University ME Aeronautical Engineering Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Aeronautical engineering, Textbooks, Reference books, Exam portions, Question Bank, Previous year question papers, Model question papers, Class notes, Important 2 marks, 8 marks, 16 marks topics.
It is applicable for all students admitted in the Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.
Anna University Chennai Syllabus
AO7011 HYPERSONIC AERODYNAMICS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, students will learn basics of hypersonic flow, shock wave -
boundary layer interaction and hypersonic aerodynamic heating.
UNIT I BASICS OF HYPERSONIC AERODYNAMICS 8
Thin shock layers – entropy layers – low density and high density flows – hypersonic flight paths
hypersonic flight similarity parameters – shock wave and expansion wave relations of inviscid
hypersonic flows.
UNIT II SURFACE INCLINATION METHODS FOR HYPERSONIC INVISCID FLOWS 9
Local surface inclination methods – modified Newtonian Law – Newtonian theory – tangent wedge
or tangent cone and shock expansion methods – Calculation of surface flow properties
19
UNIT III APPROXIMATE METHODS FOR INVISCID HYPERSONIC FLOWS` 9
Approximate methods hypersonic small disturbance equation and theory – thin shock layer theory
– blast wave theory - entropy effects - rotational method of characteristics - hypersonic shock
wave shapes and correlations.
UNIT IV VISCOUS HYPERSONIC FLOW THEORY 10
Navier–Stokes equations – boundary layer equations for hypersonic flow – hypersonic boundary
layer – hypersonic boundary layer theory and non similar hypersonic boundary layers – hypersonic
aerodynamic heating and entropy layers effects on aerodynamic heating – heat flux estimation.
UNIT V VISCOUS INTERACTIONS IN HYPERSONIC FLOWS 9
Strong and weak viscous interactions – hypersonic shockwaves and boundary layer interactions –
Estimation of hypersonic boundary layer transition- Role of similarity parameter for laminar viscous
interactions in hypersonic viscous flow.
TOTAL: 45 PERIODS
REFERENCES
1. John D. Anderson, Jr, Hypersonic and High Temperature Gas Dynamics, McGraw-Hill Series,
New York, 1996.
2. John.D.Anderson, Jr., Modern Compressible Flow with Historical perspective Hypersonic
Series.
3. William H. Heiser and David T. Pratt, Hypersonic Air Breathing propulsion, AIAA Education
Series.
4. John T. Bertin, Hypersonic Aerothermodynamics, 1994 AIAA Inc., Washington D.
AO7011 HYPERSONIC AERODYNAMICS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, students will learn basics of hypersonic flow, shock wave -
boundary layer interaction and hypersonic aerodynamic heating.
UNIT I BASICS OF HYPERSONIC AERODYNAMICS 8
Thin shock layers – entropy layers – low density and high density flows – hypersonic flight paths
hypersonic flight similarity parameters – shock wave and expansion wave relations of inviscid
hypersonic flows.
UNIT II SURFACE INCLINATION METHODS FOR HYPERSONIC INVISCID FLOWS 9
Local surface inclination methods – modified Newtonian Law – Newtonian theory – tangent wedge
or tangent cone and shock expansion methods – Calculation of surface flow properties
19
UNIT III APPROXIMATE METHODS FOR INVISCID HYPERSONIC FLOWS` 9
Approximate methods hypersonic small disturbance equation and theory – thin shock layer theory
– blast wave theory - entropy effects - rotational method of characteristics - hypersonic shock
wave shapes and correlations.
UNIT IV VISCOUS HYPERSONIC FLOW THEORY 10
Navier–Stokes equations – boundary layer equations for hypersonic flow – hypersonic boundary
layer – hypersonic boundary layer theory and non similar hypersonic boundary layers – hypersonic
aerodynamic heating and entropy layers effects on aerodynamic heating – heat flux estimation.
UNIT V VISCOUS INTERACTIONS IN HYPERSONIC FLOWS 9
Strong and weak viscous interactions – hypersonic shockwaves and boundary layer interactions –
Estimation of hypersonic boundary layer transition- Role of similarity parameter for laminar viscous
interactions in hypersonic viscous flow.
TOTAL: 45 PERIODS
REFERENCES
1. John D. Anderson, Jr, Hypersonic and High Temperature Gas Dynamics, McGraw-Hill Series,
New York, 1996.
2. John.D.Anderson, Jr., Modern Compressible Flow with Historical perspective Hypersonic
Series.
3. William H. Heiser and David T. Pratt, Hypersonic Air Breathing propulsion, AIAA Education
Series.
4. John T. Bertin, Hypersonic Aerothermodynamics, 1994 AIAA Inc., Washington D.
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