Basics of Aeronautical Engineering detailed syllabus for Electronics & Instrumentation Engineering (EIE), R18 regulation has been taken from the JNTUHs official website and presented for the students of B.Tech Electronics & Instrumentation Engineering branch affiliated to JNTUH course structure. For Course Code, Course Titles, 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 the other EIE 4th Year 1st Sem Syllabus for B.Tech R18 Regulation JNTUH scheme, visit Electronics & Instrumentation Engineering 4th Year 1st Sem R18 Scheme.
For all the (Open Elective-2) subjects refer to Open Elective-2 Scheme. The detail syllabus for basics of aeronautical engineering is as follows.
Course Objective:
- Fundamental principle of airplane
- Theoretical Aerodynamics
- Aircraft application based on speed
Course Outcome:
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Unit – I
Laws and Definitions: List the SI-units of measurement for mass, acceleration, weight, velocity, density, temperature, pressure, force, wing loading and power. – Define mass, force, acceleration and weight. – State and interpret Newtons Laws. – State and interpret Newtons first law. – State and interpret Newtons second law. – State and interpret Newtons third law. Explain air density. – List the atmospheric properties that effect air density. – Explain how temperature and pressure changes affect density. – Define static pressure. – Define dynamic pressure. – Define the formula for dynamic pressure. – Apply the formula for a given altitude and speed. – State Bernoullis equation. – Define total pressure. – Apply the equation to a Venturi. – Describe how the IAS is acquired from the pitot-static system. – Describe the relationship between density, temperature and pressure for air. – Describe the Equation of Continuity. – Define IAS, CAS, EAS, TAS
Unit – II
Basics About Airflow: Describe steady and unsteady airflow. – Explain the concept of a streamline. -Describe and explain airflow through a stream tube. – Explain the difference between two and threedimensional airflow.
Unit – III
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Unit – IV
Shape of an Aerofoil Section: Describe the following parameters of an aerofoil section: – leading edge. – trailing edge. – chord line. – thickness to chord ratio or relative thickness. – location of maximum thickness. – camber line. – camber. – nose radius. – Describe a symmetrical and an asymmetrical aerofoil section. Wing shape: Describe the following parameters of a wing: – span. – tip and root chord. – taper ratio. -wing area. – wing planform. – mean geometric chord. – mean aerodynamic chord MAC. – aspect ratio. -dihedral angle. – sweep angle. – wing twist: – geometric. – aerodynamic. – angle of incidence.
Unit – V
Subdivision of Aerodynamic Flow: List the subdivision of aerodynamic flow: – subsonic. – transonic. – supersonic flow. – Describe the characteristics of the flow regimes listed above. – Airplane for different speed and their applications.
Text Books:
For the complete syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier..
Reference Books:
- Anderson, J.D., Introduction to Flight, McGraw-Hill, 1995.
For detail syllabus of all other subjects of B.Tech Electronics & Instrumentation Engineering 4th Year 1st Sem , visit EIE 4th Year 1st Sem syllabus subjects.
For B.Tech Electronics & Instrumentation Engineering (EIE) 4th Year results, visit JNTUH B.Tech Electronics & Instrumentation Engineering semester results direct link.