Flight Investigation of Effects of Rotor-blade Twist on Helicopter Performance in the High-speed and Vertical-autorotative-descent Conditions

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Document ID

19930082289

Acquisition Source

Legacy CDMS

Document Type

Other

Authors

Date Acquired

August 16, 2013

Publication Date

August 1, 1948

Report/Patent Number

Accession Number

93R11579

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

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Type

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