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Helicopter |  |\n| --- | --- | --- | --- | --- | --- |\n| Syllabus\u003Cbr>Reference | Syllabus details & Associated Learning Objective | PPL | Bridge\u003Cbr>Course | PPL | Bridge\u003Cbr>Course |\n| [082.00.00.00](082.00.00.00) | PRINCIPLES OF FLIGHT: HELICOPTER |  |  |  |  |\n| [082.01.01.00](082.01.01.00) | Subsonic aerodynamics |  |  |  |  |\n| [082.01.01.01](082.01.01.01) | Basic concepts, laws and definitions |  |  | x | x |\n| [082.01.01.02](082.01.01.02) | Conversion of units |  |  | x | x |\n| [082.01.01.03](082.01.01.03) | Definitions and basic concepts about air: |  |  | x | x |\n|  | (a) the atmosphere and International Standard Atmosphere; |  |  | x | x |\n|  | (b) density; |  |  | x | x |\n|  | (c) influence of pressure and temperature on density. |  |  | x | x |\n| [082.01.01.04](082.01.01.04) | Newton’s laws: |  |  | x | x |\n|  | (a) Newton’s second law: Momentum equation; |  |  | x | x |\n|  | (b) Newton’s third law: action and reaction. |  |  | x | x |\n| [082.01.01.05](082.01.01.05) | Basic concepts about airflow: |  |  | x | x |\n|  | (a) steady airflow and unsteady airflow; |  |  | x | x |\n|  | (b) Bernoulli’s equation; |  |  | x | x |\n|  | (c) static pressure, dynamic pressure, total pressure and stagnation point; |  |  | x | x |\n|  | (d) TAS and IAS; |  |  | x | x |\n|  | (e) two-dimensional airflow and three-dimensional airflow; |  |  | x | x |\n|  | (f) viscosity and boundary layer. |  |  | x | x |\n| [082.01.01.06](082.01.01.06) | Two-dimensional airflow |  |  | x | x |\n| [082.01.01.07](082.01.01.07) | Aerofoil section geometry: |  |  | x | x |\n|  | (a) aerofoil section; |  |  | x | x |\n|  | (b) chord line, thickness and thickness to chord ratio of a section; |  |  | x | x |\n|  | (c) camber line and camber; |  |  | x | x |\n|  | (d) symmetrical and asymmetrical aerofoils sections. |  |  | x | x |\n| [082.01.01.08](082.01.01.08) | Aerodynamic forces on aerofoil elements: |  |  | x | x |\n|  | (a) angle of attack; |  |  | x | x |\n|  | (b) pressure distribution; |  |  | x | x |\n|  | (c) lift and lift coefficient |  |  | x | x |\n|  | (d) relation lift coefficient: angle of attack; |  |  | x | x |\n|  | (e) profile drag and drag coefficient; |  |  | x | x |\n|  | (f) relation drag coefficient: angle of attack; |  |  | x | x |\n|  | (g) resulting force, centre of pressure and pitching moment. |  |  | x | x |\n| [082.01.01.09](082.01.01.09) | Stall: |  |  | x | x |\n|  | (a) boundary layer and reasons for stalling; |  |  | x | x |\n|  | (b) variation of lift and drag as a function of angle of attack; |  |  | x | x |\n|  | (c) displacement of the centre of pressure and pitching moment. |  |  | x | x |\n| [082.01.01.10](082.01.01.10) | Disturbances due to profile contamination: |  |  | x | x |\n\n\n|  | (a) ice contamination; |  |  | x | x |\n| --- | --- | --- | --- | --- | --- |\n|  | (b) ice on the surface (frost, snow and clear ice) . |  |  | x | x |\n| [082.01.01.11](082.01.01.11) | The three-dimensional airflow round a wing and a fuselage |  |  | x | x |\n| [082.01.01.12](082.01.01.12) | The wing: |  |  | x | x |\n|  | (a) planform, rectangular and tapered wings; |  |  | x | x |\n|  | (b) wing twist. |  |  | x | x |\n| [082.01.01.13](082.01.01.13) | Airflow pattern and influence on lift: |  |  | x | x |\n|  | (a) span wise flow on upper and lower surface; |  |  | x | x |\n|  | (b) tip vortices; |  |  | x | x |\n|  | (c) span-wise lift distribution. |  |  | x | x |\n| [082.01.01.14](082.01.01.14) | Induced drag: causes and vortices |  |  | x | x |\n| [082.01.01.15](082.01.01.15) | The airflow round a fuselage: |  |  | x | x |\n|  | (a) components of a fuselage; |  |  | x | x |\n|  | (b) parasite drag; |  |  | x | x |\n|  | (c) variation with speed. |  |  | x | x |\n| [082.02.01.00](082.02.01.00) | Transonic aerodynamics and compressibility effects |  |  |  |  |\n| [082.02.01.01](082.02.01.01) | Airflow velocities |  |  | x | x |\n| [082.02.01.02](082.02.01.02) | Airflow ","cbCaitMdofrg7R1t","https://ap.wps.com/l/cbCaitMdofrg7R1t","pdf",717363,"English","# Principles of Flight: Helicopter (082)\n## Subsonic aerodynamics\n## Transonic aerodynamics and compressibility effects\n## Rotorcraft types and helicopter configurations\n## Helicopter terminology and components\n## Main rotor aerodynamics","[{\"question\":\"What major aerodynamics topics are covered in 082 Principles of Flight: Helicopter?\",\"answer\":\"The syllabus covers subsonic aerodynamics and key fundamentals such as atmosphere and density, Newton’s laws, airflow concepts, and lift and drag, then extends to transonic aerodynamics and compressibility effects including shock waves.\"},{\"question\":\"Which rotorcraft and helicopter configuration subjects are included?\",\"answer\":\"It lists rotorcraft types, autogyro and helicopter basics, helicopter configurations (including the single main rotor helicopter), and an overview of helicopter characteristics and associated terminology.\"},{\"question\":\"What does the syllabus say about main rotor aerodynamics?\",\"answer\":\"It includes hover flight outside ground effect and describes airflow through the rotor discs and around the rotor blades, as part of the main rotor aerodynamics objectives.\"}]","Private Pilot Licence Examinations - 082 Principles of Flight Helicopter - Learning objectives | PDF",1790319346,18]