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Attached is the Ka-50 hovering on a calm, no-wind day and the rotor blade disk seems to be tilting at approximately 3-5 degrees. What could be causing this *much* tilt?

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  • 3 weeks later...
Posted
On 11/8/2023 at 6:30 AM, Sarix said:

Attached is the Ka-50 hovering on a calm, no-wind day and the rotor blade disk seems to be tilting at approximately 3-5 degrees. What could be causing this *much* tilt?

P{I`S7OF{VCM6`OF[75O47I.png

Most helicopters hover nose high, Mi-8/24 can be anywhere from 0-6 degrees depending weight. Apache is I think around 4-6 degrees. 
 
A helicopter needs to pitch the nose for in order to maintain forward speed, you want to design a helicopter to fly at cruise speed efficiently. Right now Ka-50 flies in cruise about nose level. If it didn’t hover nose high, it would need 3-5 degrees nose down in cruise. At such an amount of nose down, fuselage/wing drag increases and wing produces negative lift. 
 

That is, if I understand your question correctly that it’s about nose angle not the actual rotor disk tilting. 

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Posted
7 hours ago, AeriaGloria said:

Most helicopters hover nose high, Mi-8/24 can be anywhere from 0-6 degrees depending weight. Apache is I think around 4-6 degrees. 
 
A helicopter needs to pitch the nose for in order to maintain forward speed, you want to design a helicopter to fly at cruise speed efficiently. Right now Ka-50 flies in cruise about nose level. If it didn’t hover nose high, it would need 3-5 degrees nose down in cruise. At such an amount of nose down, fuselage/wing drag increases and wing produces negative lift. 
 

That is, if I understand your question correctly that it’s about nose angle not the actual rotor disk tilting. 

It was indeed about the rotor disk proper. But the answer is appreciated too! Do you think the rearwards tilt of the rotor disk (relative to the ground) is related to this?

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  • 3 weeks later...
Posted
On 11/29/2023 at 10:14 PM, Sarix said:

It was indeed about the rotor disk proper. But the answer is appreciated too! Do you think the rearwards tilt of the rotor disk (relative to the ground) is related to this?

No, but the wing is at 6 degrees incidence and thus produces a slight thrust forward from the rotor downwash. The rearward tilt probably Atleast partially overcomes this 

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Posted

Keep in mind, that the center of gravity isn't necessarily directly below the rotor shaft (it is shifted aft, I think) and that the rear side of the rotordisc probably produces more lift.

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