Actions for The Effects on the Aerodynamic Characteristics of Varying the Wing Thickness Ratio of a Triangular Wing-body Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method

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The Effects on the Aerodynamic Characteristics of Varying the Wing Thickness Ratio of a Triangular Wing-body Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method

Author
Mckay, James M
Published
April 2, 1952.
Physical Description
1 electronic document
Additional Creators
Hall, Albert W
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: 19930087023.
Accession ID: 93R16313.
NACA-RM-L52B18.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15431115