Gilles Louis - Dynamics of Aircraft Flight

The velocity of an aircraft is often given by the Mach number. This value is the ratio at a specific point between the velocity of the flow V and the speed of sound at that point. The “aircraft” Mach number is the ratio M 0between the aerodynamic velocity V 0(relative velocity of the airplane with respect to the air, assumed, for example, to be stationary at infinity) and the speed of sound at infinity upstream a 0.

The mechanics of flight immediately bring to mind the trajectory of aircraft and the catastrophic consequences that human errors or computer calculation errors can have on flight safety. The crash of the Indonesian Lion Air (October 2018) and Ethiopian Airlines (March 2019) Boeing 737 Max aircraft led to the deaths of 346 innocent people and a shutdown of around 800 such aircraft around the world.

A US Congress report highlights the heavy financial pressure on Boeing and the 737 Max program to get ahead of the release of Airbus’ new aircraft, the A320 Neo, which affected the MCAS collision avoidance system implicated in the two accidents, as well as the culture of concealment that prevailed in the manufacturer and that prevented it from sharing crucial information with the authorities, its customers and the pilots of the 737 Max.

We must learn from the consequences of these disasters in order to prevent them from happening again, and engineers have a major role to play, in the sense that they are the guarantors of the safety and reliability of manufactured aircraft and must do everything possible to manage risks in order to minimize the occurrence of such disasters.

NOTE.– The units used in this book are those of the international metric system.

Let us use the direct trihedron defined in Figure I.1.

Figure I.1. Direct trihedron

Thus, the pitch, roll and yaw axes are defined as follows.

Figure I.2. Roll axis (rotation around the X axis)

Figure I.3. Yaw axis (rotation around the Z axis)

Figure I.4. Pitch axis (rotation around the Y axis)

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