Aerodynamic Characteristics of the NACA 8-H-12 Airfoil Section at Six Reynolds Numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6). - NASA Technical Reports Server (NTRS)

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Aerodynamic Characteristics of the NACA 8-H-12 Airfoil Section at Six Reynolds Numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).

Document ID

19930082712

Acquisition Source

Legacy CDMS

Document Type

Other

Authors

Date Acquired

August 16, 2013

Publication Date

December 1, 1949

Report/Patent Number

Accession Number

93R12002

Distribution Limits

Public

Copyright

Work of the US Gov. Public Use Permitted.

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