Actions for High-speed Tests of an Airfoil Section Cambered to Have Critical Mach Numbers Higher than Those Attainable with a Uniform-load Mean Line

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High-speed Tests of an Airfoil Section Cambered to Have Critical Mach Numbers Higher than Those Attainable with a Uniform-load Mean Line

Author
Graham, Donald J
Published
July 1947.
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: 19930082040.
Accession ID: 93R11330.
NACA-TN-1396.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15435342