UniCopter ~
Vibration - Rotor Induced - AnalysisOverview:
An attempt to try to;
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1. Potential Sources of Vibration: |
ID |
Hover: |
Transition: μ ≈ 0.1? |
High Speed |
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Dissymmetry of lift (and drag?). |
19/ |
No |
No |
Yes |
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Rotor to Rotor (downwash & downdraft) |
17/ |
Yes |
Yes |
Yes |
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Blade to Blade (BVI) (within same rotor) |
12/ |
Maybe |
Yes |
No |
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Rotor to Rotor (BVI) (between blades of different rotors) |
18/ |
Maybe |
Maybe |
Maybe |
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Downwash on the Fuselage. |
1/ |
No |
No |
Yes |
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Downwash on the Tail Boom. |
2/ |
Yes |
Yes |
Yes |
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Gusts. |
14/ |
Yes |
Yes |
Yes |
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Moments about the blades' feathering axes. |
15 & 16/ |
Yes |
Yes |
Yes |
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A primary index of ID's above can be found on pages; 1020.html & 1089.html |
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Working Papers:
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DESIGN: |
MAKE: |
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BUY: |
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Items:
DESIGN:
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Name |
Item |
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General: |
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Source - Individual Rotor: (aerodynamic vibrations on an independent rotor.) |
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UniCopter ~ Vibration - Rotor Induced - Analysis - Blades to Hubs |
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UniCopter ~ Rotor - Disk - Single - Downwash in Hover |
0887 |
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17/ |
Source - Rotor to Rotor: (vibrations inflicted on one rotor by the other.) |
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UniCopter ~ Rotor - Disk - Aerodynamic Interaction between Intermeshing Disks |
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UniCopter ~ Rotor - Disk - Clearance - 3 Blades RRR |
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UniCopter ~ Rotor - Disk - Downwash Intersection Azimuths |
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19/ |
Source - Lateral Dissymmetry of Lift (and Drag?): (vibrations from uneven thrust.) |
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UniCopter ~ Rotor - Disk - Lateral Dissymmetry of Lift |
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1/ & 2/ |
Source - Fuselage: (downwash on fuselage and tail boom) |
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UniCopter ~ Vibration - Rotor Induced - Analysis - Downwash on Fuselage |
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15 & 16/ |
Source - Cyclic Stick from Individual Rotor via Pitch Links: |
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OTHER:
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Name |
Item |
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OTHER: Aerodynamics - Vibration - Rotor Induced |
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~ or ~ |
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OTHER: Aerodynamics - Vibration - Rotor Induced - Overview |
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OTHER: Aerodynamics - Vibration - Rotor Induced - Source- Single Rotor |
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OTHER: Aerodynamics - Vibration - Rotor Induced - Source - Twin Rotor |
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12 & 18/ |
OTHER: Aerodynamics - Vibration - Rotor Induced - Blade Vortex Interaction [BVI] |
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OTHER: Aerodynamics - Vibration - Rotor Induced - Re: Coaxial (Sikorsky ABC & Kamov) |
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OTHER: Aerodynamics - Vibration - Rotor Induced - Re: Flettner FL-282 |
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Last Revised: April 7, 2004