Actions for Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area IV : Some Effects of Internal Duct Shape upon an Inlet Enclosing 37.2 Percent of the Forebody Circumference

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Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area IV : Some Effects of Internal Duct Shape upon an Inlet Enclosing 37.2 Percent of the Forebody Circumference

Author
Edwards, Sherman S
Published
March 15, 1949.
Physical Description
1 electronic document
Additional Creators
Brajnikoff, George B and Davis, Wallace F
Online Version

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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: 19930085928.
Accession ID: 93R15218.
NACA-RM-A9A31.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15432047