FUNDAMENTAL OF AEROSPACE ENGINEERING
Course Objective:
To provide basic concepts of Aerospace Engineering. Various fields within the field of aerospace engineering.
- Standard Atmosphere (2 hours)
- Derive the formulation for the standard atmosphere, including the various altitude definitions.
- Define pressure, temperature and density altitude.
- Use standard atmosphere tables.
- Perform standard atmosphere calculations
- Aero/Hydrodynamics (4 hours)
- Define viscosity and discuss its implications.
- Calculate the shear stress at a point given a velocity profile.
- Define the Lagrangian and Eulerian viewpoints of a flow field.
- Define the concept of a streamline.
- Apply conservation of mass to a control volume.
- Use Bernoulli’s equation to calculate pressures and velocities in a flow field.
- Wing Geometry (6 hours)
- Define common aircraft terminology and geometry.
- Identify basic aircraft types and discuss their features.
- Define and calculate the lift and drag coefficients using NACA data.
- Define and interpret CL vs. alpha, and CL vs CD curves for 2-D wing sections.
- Explain the difference between 2D sections and 3D wings.
- Performance and Propulsion (6 hours)
- Describe the viscous and pressure drag components on a body.
- Define flow separation and explain where it might occur.
- Explain the three types of aerodynamic drag.
- Perform lift and drag calculations on aircraft.
- Perform thrust calculations.
- Define the thrust/power available and thrust/power required flight envelope.
- Describe how this flight envelope changes with altitude, including the ceiling.
- Aircraft Stability (6 hours)
- Define the six degrees of freedom of aircraft motions.
- Define stable, unstable and neutral stability.
- Explain the difference between static and dynamic stability.
- Explain what is meant by static longitudinal stability for aircraft.
- Explain coupling in lateral and directional stability.
- Structural Theory (10 hours)
- Define what is meant by a neutral axis.
- Define stress and strain and their relationship via Hooke’s Law.
- Draw a typical stress-strain diagram for brittle and ductile materials and introduce yielding and fracture.
- Calculate the moment of inertia of a beam’s cross-section.
- Solve for the stress distribution over a beam’s cross-section.
- Define and calculate a section modulus.
- Aircraft Structure (4 hours)
- Describe the function of the primary load carrying members.
- Perform a spar cap sizing example.
- Understand the basic V-n diagram.
- Space Applications (7 hours)
- Discuss the history of space research.
- Define orbital motion including typical spacecraft trajectories and basic orbital maneuvers.
- Define the six orbital elements.
- Understand and be able to apply Kelper’s laws of orbits.
- Understand and be able to apply Newtons law of gravitation.
Practical
- Lab for conceptual design works based on clay model and CAD.
- Summarized on research article related to current advancement in Aerospace Technologies.
References
- Flight without Formulae by A.C Kermode, Pearson Education, 10th Edition
- Mechanics of Flight by A.C Kermode, Pearson Education, 5th Edition
- Fundamentals of Flight, Shevell, Pearson Education, 2nd Edition
- Introduction to Flight by Dave Anderson
- Aircraft systems: Mechanical,Electrical&Avionics subsystems integration by lanmoir, Allen Seabridge.
Evaluation Scheme:
The questions will cover all the chapters of the syllabus. The evaluation scheme will be as indicated in the table below:
Unit |
Chapter |
Topics |
Marks |
1 |
1 & 2 |
All |
16 |
2 |
3&4 |
All |
16 |
3 |
5 |
All |
16 |
4 |
6 & 7 |
All |
16 |
5 |
8 |
All |
16 |
Total |
80 |
*Note: There may be minor deviation in marks distribution
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