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2.Helicopter Momentum Theory(Actuator Disk)
Answer:
• The details of the flow around the blades are not considered.
• Rotor is considered as an actuator disk (infinite number of infinitesimal small blades) which
adds momentum and energy to the flow.
• Incompressible flow.
• Steady, inviscid(no dissipation), and irrotational flow.
• Flow is 1-D, and uniform through the rotor disk, and in the far wake.(don't need to consider the details in the flow enviroment)
• No swirl in the wake.
• No tip vorticies.
• Well defined slipstream.
• The far stream is at ambient pressure.
The basic principles applied by the actuator disk theory are the mass, momentum, and energy balance equations that we already know must be valid for any material volume.
本题图片内容感谢Marco Fiorito先生的支持
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