Aerodynamics & Performance
Aerodynamics is the branch of dynamics dealing with the motion of air and other gases that provide the performance aircraft need to fly.
Introduction
Introduction
- Aerodynamics is the branch of dynamics dealing with the motion of air and other gases, which gives us the performance we need to fly.
- Understanding basic aerodynamic concepts is essential to understanding the operation of the components and subcomponents of an aircraft.
- The principal aerodynamic concepts are that of the four forces that affect aircraft.
- It can be associated with the forces acting on an object in motion through the air or with a stationary object in a current of air.
- Several factors affect aircraft performance, including the atmosphere, aerodynamics, and aircraft icing.
- Pilots need an understanding of these factors to provide a sound basis for anticipating aircraft response to control inputs, which come in the form of performance.
Lift and Basic Aerodynamics
Lift and Basic Aerodynamics
- Aircraft Components and Structure create the physical form we know as an aircraft.
- Four forces act upon an aircraft, making up the Principles of Flight.
- Understanding how these forces are created and, more importantly, impact each other allows pilots to control an aircraft in flight.
- These principle forces are thrust, drag, weight, and lift: [Figure 1]
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Thrust:
- Thrust is the forward force produced by the powerplant/propeller.
- It opposes or overcomes the force of drag.
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Drag:
- Drag is a rearward, retarding force caused by disruption of airflow by the wing, fuselage, and other protruding objects.
- Drag opposes thrust and acts rearward parallel to the relative wind.
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Weight:
- Weight is the combined load of the aircraft itself, the crew, the fuel, and the cargo or baggage.
- The weight pulls the aircraft downward because of the force of gravity.
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Lift:
- Lift opposes the downward force of weight, produced by the dynamic effect of the air acting on the wing and acts perpendicular to the flight path through the wing's center of lift (CL).
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- Engineers design aircraft with different handling characteristics in mind, which determine aircraft stability.
- An aircraft moves in three dimensions and is controlled by moving it about one or more of its axes:
- The longitudinal, or roll, axis extends through the aircraft from nose to tail, with the line passing through the center of gravity.
- The lateral or pitch axis extends across the aircraft on a line through the wing tips, again passing through the center of gravity.
- The vertical, or yaw, axis passes through the aircraft vertically, intersecting the center of gravity.
- All control movements cause the aircraft to move around one or more of these axes and allow for the control of the aircraft in flight. [Figure 3]
- Aircraft performance designs are dependent upon operating within weight and balance limitations.
- NASA - Aerodynamics Index
Aircraft Performance
Aircraft Performance
- The performance or operational information section of the Aircraft Flight Manual/Pilot's Operating Handbook (AFM/POH) contains the aircraft's takeoff, climb, range, endurance, descent, and landing data.
- Using this data in flying operations is mandatory for safe and efficient operation.
- Pilots gain considerable knowledge and familiarity with the aircraft through the study of this material:
Aircraft Performance Charts, Tables, and Data
Aircraft Performance Charts, Tables, and Data
- Aircraft performance is tested under specific conditions that are later compiled in performance charts
- Pilots must reference these performance charts to calculate the anticipated performance for a given operation
- Calculate crosswind component for takeoff and landing
- Calculating short-field takeoff and climb distance
Performance Calculations Versus Reality
Performance Calculations Versus Reality
- Charts contain performance data based on expected performance under a set of conditions.
- Said differently, pilot operating handbook numbers require the pilot operating handbook technique.
- The conditions present during calculation will always differ from the charts and graphs to a degree, sometimes a large degree.
- Factors to consider include mechanical, environmental, skill, geographic location or altitude, etc.
- It is important to use conservative numbers.
- Consider always rounding up, not interpolating but using the higher number, etc.
- Realize obstacles like trees may be more than 50'; therefore, charts are wholly inadequate to calculate by numbers.
- Consider adding 50-100% buffers to anything calculated and monitor performance while in flight.
- If numbers were overly conservative, adjust for subsequent flights.
Conclusion
Conclusion
- Resources like Real Engineering - The Plane That Will Change Travel Forever describe complex aerodynamical topics clearly and concisely.
- Consider actual versus realized performance when doing any performance calculations.
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References
References