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Title
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A Stability and Control Prediction Method for Helicopters and Stoppable Rotor Aircraft. Volume I. Engineer's Manual
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Date
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1970
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Index Abstract
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Coming Soon
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Photo Quality
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Not Needed
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Report Number
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AFFDL TR 69-123 Volume 1
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Corporate Author
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Bell Helicopter Company
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Laboratory
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Air Force Flight Dynamics Laboratory
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Extent
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86
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Identifier
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AD0707881
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Access Rights
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This document has been approved for public release and sale; its distribution is unlimited
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Distribution Classification
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1
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Contract
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F33615-69-C-1121
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DoD Project
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8219
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DTIC Record Exists
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No
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Distribution Change Authority Correspondence
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None
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Abstract
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This report describes a mathematical model of rotorcraft that may be used to determine characteristics of performance, stability, response, and rotor blade loads. The complexity of the equations used requires the use of a digital computer for efficient solution. This four volume report describes the computer program in detail and illustrates the method of computing rotorcraft characteristics by specific example.
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Report Availability
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Full text available
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Date Issued
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1970-02
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Provenance
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AFRL/VACA
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Type
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report
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Format
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1 online resource
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Creator
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Livingston, Charles L.
