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Scale-effect tests in a turbulent tunnel of the NACA 65(sub 3)-418, a = 1.0 airfoil section with 0.20-airfoil-chord split flap

Author
Wallace, Arthur R
Published
September 1944.
Physical Description
1 electronic document
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930092796.
Accession ID: 93R22086.
NACA-ACR-L4I22.
NACA-WR-L-128.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15664817