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Actions for An integrating manometer for use in wind tunnel pressure distribution measurements
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An integrating manometer for use in wind tunnel pressure distribution measurements
Author
Noyes, Richard W
Physical Description
1 electronic document
Online Version
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Unclassified, Unlimited, Publicly available.
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Summary
A multiple manometer designed to integrate automatically the normal force over an airfoil section is described and its mathematical theory explained. The development of this instrument was conducted at the Langley Memorial Aeronautical Laboratory.
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930081200.
Accession ID: 93R10490.
NACA-TN-377.
Terms of Use and Reproduction
No Copyright.
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