Tests in the Ames 40- by 80-foot Wind Tunnel of an Airplane Configuration with a Variable-incidence Triangular Wing and an All-movable Horizontal Tail - NASA Technical Reports Server (NTRS)

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Tests in the Ames 40- by 80-foot Wind Tunnel of an Airplane Configuration with a Variable-incidence Triangular Wing and an All-movable Horizontal Tail

Document ID

19930087582

Acquisition Source

Legacy CDMS

Document Type

Other

Authors

Date Acquired

August 16, 2013

Publication Date

June 25, 1953

Report/Patent Number

Accession Number

93R16872

Distribution Limits

Public

Copyright

Work of the US Gov. Public Use Permitted.

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19930087582.pdf

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