NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Determination of the profile drag of an airplane wing in flight at high Reynolds numbers
Document ID
19780078526
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bicknell, J. (National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1939
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-79838
NACA-TR-667
Accession Number
78N78519
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available