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The thrust forces in an engine are the gas loads which result from the pressure and momentum changes of the gas stream reacting on the engine structure and its rotating components. Some are forward and some are rearward forces. The excess of the forward forces over the rearward force is known as the rated thrust of an engine. Chapter 2 Page 1 © G LONGHURST 1999 All Rights Reserved Worldwide Engine Performance 5. Engine thrust is displayed on a gauge as engine pressure ratio (EPR). The pilot selects the appropriate EPR by adjusting the thrust levers.

This is the absolute ceiling, which is of little practical use because it is a long slow process to reach it. See Figure 1-18 and Figure 1-19. 5m/s) for propeller driven aeroplanes. Chapter 1 Page 33 © G LONGHURST 1999 All Rights Reserved Worldwide Basic Aerodynamics FIGURE 1-17 The Effect of Altitude. Example Approximately 10,000 ft Chapter 1 Page 34 © G LONGHURST 1999 All Rights Reserved Worldwide Basic Aerodynamics FIGURE 1-18 Example Approximately 20,000 ft Chapter 1 Page 35 © G LONGHURST 1999 All Rights Reserved Worldwide Basic Aerodynamics FIGURE 1-19 Effect of Altitude on Power Available (Jet) The Buffet Onset Boundary Chart 23.

Chapter 1 Page 32 © G LONGHURST 1999 All Rights Reserved Worldwide Basic Aerodynamics Aircraft Ceiling. At the point at which the power available curve only just touches the power required curve a climb is no longer possible. Furthermore there is only one speed possible in level flight. This is the absolute ceiling, which is of little practical use because it is a long slow process to reach it. See Figure 1-18 and Figure 1-19. 5m/s) for propeller driven aeroplanes. Chapter 1 Page 33 © G LONGHURST 1999 All Rights Reserved Worldwide Basic Aerodynamics FIGURE 1-17 The Effect of Altitude.

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Aeroplane Performance Tutorial - PPSC


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