Actions for Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area I : an Inlet Enclosing 61.5 Percent of the Maximum Circumference of the Forebody

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Experimental Investigation at Supersonic Speeds of Twin-scoop Duct Inlets of Equal Area I : an Inlet Enclosing 61.5 Percent of the Maximum Circumference of the Forebody

Author
Goldstein, David L
Published
January 21, 1948.
Physical Description
1 electronic document
Additional Creators
Davis, Wallace F
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: 19930085760.
Accession ID: 93R15050.
NACA-RM-A7J27.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15432202