This document provides an overview of topics covered in an aerospace engineering tutorial, including: 1. Applied solid mechanics concepts such as stress, strain, and analyzing statically indeterminate structures. 2. Instrumentation and measurement techniques for recording data like strain, pressure, temperature and flow. 3. Aerothermodynamics principles involving hypersonics, aerodynamics, gas dynamics, and heat transfer. 4. Introduction to spacecraft dynamics and numerical methods.

1. Aerospace Engineering
Tutorial-1 by Awwal

2. CONTENT
• Introduction
• Applied Solid Mechanics
• Instrumentation and Measurements
• Aerothermodynamics of Flows
• Introduction to spacecraft dynamics
• Numerical Methods and Data science to Engineering
• Control system analysis and design
• Subsonic Aerodynmaics and Wings

3. Applied Solid Mechanics
• Equilibrium of forces and continuity of displacements
• The basic concepts of stress and strain
• Free body diagrams and their use in analysis techniques
• The mechanical principles related to design of struts, tie-bars, shafts and pressure
vessels
• Thermally induced stresses and strains
• Solution techniques for statically indeterminate structures
• Analysis techniques for assessing the deflection and stress within simple beams
• Principal stresses and maximum shear stresses

4. Introduction
Applied Solid Mechanics
Strength of Materials is a fundamental subject needed primarily for the Mechanical sciences. As the engineering
design of different components, structures etc. used in practice are done using different kinds of materials, it is
essential to understand the basic behavior of such materials. The Material that is used in Aerospace, Perhaps it
deals firstly with the effect of machining technology on structure of Aerospace Material.
The Four principles of Mechanics of Material are:
1.Free Body Diagram. If a part is separated or isolated from a body (ie: sectioned) or surroundings (ie: boundary
conditions), appropriate reactions and/or internal forces must be added.
2.Equilibrium of Forces. If a part or body is in equilibrium, all reactions and/or internal forces must also be in
equilibrium.
3.Displacement Compatibility. The nature of plausible deformation in a system imposes constraints on the geometry
and/or deformation of structural elements in a given system (ie: two solid objects cannot occupy the same space,
elements rigidly connected to each other must deform with each other).
4.Stress-Strain (Force-Displacement) Relations. Loading and deformation in a structure are linked by material
properties and structural geometry through Hooke’s Law

5. Applied Solid Mechanics
Material Affect the following aspects:
A)Performance Parameters (Range, Velocity, Capacity)
B)Reliability
C)Safety
D)Engine Power
E)Components of structures
F)Fuel Consumption

6. • Instrumentation and
Measurements
• Fundamentals of measurement
systems; standards; dynamic
characteristics of instruments;
statistical data treatment;
transducers; signal conditioning;
strain, pressure, temperature
and flow measurements.

8. • Aerothermodynamics of Flows
• hypersonics, aerodynamics, gas dynamics, turbulence, plasma
dynamics, heat transfer, and combustion.

9. • Introduction to spacecraft dynamics

10. Introduction
• Numerical Methods and Data
science to Engineering

11. • Control system analysis and design

12. • Subsonic Aerodynmaics and Wings