NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Acoustic response function equation for a T- burner with high heat loss.Solid propellants acoustic response function in T-burners, analyzing effect of decreased sonic velocity
Document ID
19680042164
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Dehority, G. L.
Mathes, H. B.
Date Acquired
August 4, 2013
Publication Date
April 1, 1968
Publication Information
Publisher: AIAA JOURNAL, VOL. 6, P. 741, 742.
Subject Category
Thermodynamics And Combustion
Accession Number
68A23136
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available