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Experimental investigation of an acoustic liner with variable cavity depth

Author
Phillips, B.
Published
Apr 1, 1968.
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
Summary
Hydrogen-oxygen rocket engine used to test acoustic liner with isolated resonators and variable cavity depths
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19680012211.
Accession ID: 68N21680.
NASA-TN-D-4492.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15955445