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A method for the surface installation and fairing of static-pressure orifices on a large supersonic-cruise airplane

Author:
Taillon, N. V.
Published:
Mar 1, 1968.
Physical Description:
1 electronic document
Online Version

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Restrictions on Access:
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary:
Installation and fairing of flush, static pressure orifices on wing surfaces of supersonic aircraft
Other Subject(s):
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 19680009872.
Accession ID: 68N19341.
NASA-TM-X-1530.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15955598