Lecture 2 - Introduction to International Standard Atmosphere (ISA) PDF

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Punjab Engineering College, Chandigarh

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International Standard Atmosphere aerospace vehicles atmospheric science altitude types

Summary

This lecture provides an introduction to the International Standard Atmosphere (ISA), discussing aerospace vehicles, different altitude types (geometric, absolute, geopotential, pressure, temperature, and density), and relevant formulas like the hydrostatic equation. It also touches on the composition and layers of the Earth's atmosphere.

Full Transcript

# Lecture No. 01.2: Introduction to International Standard Atmosphere (ISA) ## Aerospace Vehicles The main categories of aerospace vehicles are: - **Atmospheric vehicles**: Vehicles which fly in the Earth's atmosphere only, such as: - Helicopters - Airplanes - **Space vehicles:** Vehicles...

# Lecture No. 01.2: Introduction to International Standard Atmosphere (ISA) ## Aerospace Vehicles The main categories of aerospace vehicles are: - **Atmospheric vehicles**: Vehicles which fly in the Earth's atmosphere only, such as: - Helicopters - Airplanes - **Space vehicles:** Vehicles which fly in deep space, such as: - Satellites ## Why do we need ISA? - **ISA** (International Standard Atmosphere) is a hypothetical model utilized for: - Design and performance determination for aerospace vehicles - Simulation and Analysis - Relating flight test and wind tunnel results to a common reference for aircraft design and performance - It provides a constant model in lieu of the variable characteristic of the actual Earth's atmosphere. ## What are these different altitudes? - **Geometric altitude**: Measured as vertical distance from mean sea level. It is also known as **true altitude**. - **Absolute altitude**: Measured as vertical distance from the center of the Earth. - **Geopotential altitude**: A variation in gravitational acceleration (g) is considered with respect to altitude. This concept is applied only for space vehicles. - **Pressure altitude**: Measured based on the pressure at a specific altitude. - **Temperature altitude**: Measured based on the temperature at a specific altitude. - **Density altitude**: Measured based on the density at a specific altitude. For the study of atmospheric vehicles, the *geometric altitude* is used for now. The other 5 types of altitudes will be studied in later lectures. ## Indicated Altitude - Indicated altitude is what the pilot sees on the altimeter, as shown in the image of an aircraft cockpit. ## True altitude - True altitude is the geometric altitude, measured as the vertical distance above mean sea level. ## Absolute Altitude - Absolute altitude is the distance from the center of the earth to the specific altitude. This is related to the geometric altitude and radius of the Earth with the formula: $h_a = h_g + r$. - See figure with diagram of a spherical earth. ## Geopotential Altitude - Geopotential altitude takes into account the variation of gravitational acceleration (g) with altitude. - The formula is: $g = g_0 * (r/h_a)² = g_0 *(r/r+h_g)²$. - The formula defines $h$ (geopotential altitude) as: $h = \frac{rh_g}{r+h_g}$ - Geopotential altitude is used for calculation related to space vehicles only. ## Hydrostatic Equation - The hydrostatic equation models the force balance of a fluid element at rest in a gravitational field. - The equation is $p = p + dp + \rho g dh_g$ - The derivative form of the equation is $dp = - \rho g dh_g$ ## LAYOUT - This lecture covers Earth's atmosphere, and related atmospheric standards - It introduces the various types of altitudes - It introduces the two main equations for calculating pressure and density of a fluid element at rest. - It discusses Q code standards used to communicate altitudes in air traffic control communication. - It will be followed by another lecture on the effects of weather. ## Atmosphere - Earth's atmosphere is a blanket of air surrounding the planet. - It is essential to support life on Earth. - The composition of the atmosphere is mainly: - Oxygen ($O_2$): 21% - Nitrogen ($N_2$): 78% - Others: 1% ## Layers of the Atmosphere - The Earth's atmosphere can be divided into several layers, which can be described as the "layers of the atmosphere". - They are: - **Troposphere**: The lowest layer, where most weather phenomena occur. - **Stratosphere**: Contains the ozone layer, which absorbs harmful ultraviolet radiation from the Sun. - **Mesosphere**: The coldest layer of the atmosphere. - **Thermosphere**: The hottest layer, where the temperature increases with altitude due to the absorption of solar radiation. - **Ionosphere**: A region in the upper thermosphere where atoms and molecules are ionized by solar radiation. - **Exosphere**: The outermost layer of the atmosphere, where the atmosphere gradually fades into space. ## AEROSPACE VEHICLES (continued) - This section explores the different types of aerospace vehicles. - The goal is to understand **why we study these vehicles**. - Through this study, we can investigate their design and performance characteristics.

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