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Accession Number
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AVA16929-VM00
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Title
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Helicopter Aerodynamics - The Stabilizer Bar.
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Publication Date
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1994
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Media Count
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1AV-Beta 2 - 1 cassette
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Personal Author
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N/A
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Abstract
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Shows how the gyroscope properties of the bar affect stabilizer helicopter operation. Shows the effect of rigidity in space on the rotor and fuselage. Shows the function of the damper assembly.
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Keywords
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Aerodynamics Audivisual aids Helicopters Rotor blades(Rotary wings)
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Source Agency
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Department of the Army - Audiovisual
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NTIS Subject Category
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51C - Aircraft 51A - Aerodynamics
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Corporate Author
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Department of the Army, Washington, DC.
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Document Type
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Audiovisual
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Title Note
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N/A
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NTIS Issue Number
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0003
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Contract Number
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N/A
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