Investigation of Slipstream Effects on a Wing-inlet Oil-cooler Ducting System of a Twin-engine Airplane in the Ames 40- by 80-foot Wind Tunnel

Press Enter or click the Search button to begin your search.

Document ID

19930093542

Acquisition Source

Legacy CDMS

Document Type

Other

Authors

Date Acquired

September 6, 2013

Publication Date

March 10, 1945

Report/Patent Number

Accession Number

93R22832

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

Name

Type

STI

No Preview Available

NTRS