High Speed Aerodynamics detailed Syllabus for Aeronautical Engineering (AERO), R18 regulation has been taken from the JNTUH official website and presented for the students affiliated to JNTUH course structure. For Course Code, Subject Names, Theory Lectures, Tutorial, Practical/Drawing, Credits, and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the universities official website.
For all other AERO 3rd Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH, do visit AERO 3rd Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH Subjects. The detailed Syllabus for high speed aerodynamics is as follows.
Pre-requisite:
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Course Objectives:
- Understand the effect of compressibility at high-speeds and the ability to make intelligent design decisions.
- Explain the dynamics in subsonic, transonic and supersonic flow regimes in both internal and external geometries.
- Analyze the airfoils at subsonic, transonic and supersonic flight conditions using the perturbed flow theory assumption.
- Formulate appropriate aerodynamic models to predict the forces and performance of realistic three-dimensional configurations.
Course Outcomes:
- Air compressibility and isentropic relations inform of speed
- Shock and expansion waves,
- Supersonic wind tunnel, nozzle design, flow visualisation technique
Unit I
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Unit II
Shock And Expansion Waves:
Shocks and expansion waves: Development of governing equations for normal shock, stationery and moving normal shock waves, applications to aircrafts, supersonic wind tunnel, shock tubes, shock polars, supersonic pitot probes; oblique shocks, governing equations, reflection of shock, Prandtl-Meyer expansion flow, shock expansion method for flow over airfoil, introduction to shock wave boundary layer interaction.
Unit III
One Dimensional And Quasi One-Dimensional Flow:
Quasi one-dimensional flow: Isentropic flow in nozzles, area Mach relations, choked flow, under and over expanded nozzles, slip stream line. One dimensional flow: Flow in constant area duct with friction and heat transfer, Fanno flow and Rayleigh flow, flow tables and charts for Fanno flow and Rayleigh flow.
Unit IV
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Unit V
Experimental Methods In Compressible Flows:
Experimental methods: Subsonic wind tunnels, supersonic wind tunnels, shock tunnels, free-piston shock tunnel, detonation-driven shock tunnels, and expansion tubes and characteristic features, their operation and performance, flow visualization techniques for compressible flows.
Text Books:
- John D. Anderson, Modern Compressible flow with historical perspective!, McGraw-Hill Education, 3rd Edition, 2002.
- John D. Anderson, Fundamentals of Aerodynamics!, McGraw-Hill Education, 6th Edition, 2016.
Reference Book:
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For detail Syllabus of all other subjects of B.Tech 3rd Year Aeronautical Engineering, visit AERO 3rd Year Syllabus Subjects.
For all B.Tech results, visit JNTUH B.Tech all years, and semester results from direct links.