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Effect of injection element radial distribution and chamber geometry on acoustic mode instability in a hydrogen oxygen rocket [NASA TN D-5375]

By: Material type: TextTextLanguage: English Series: National Aeronautics and Space Administration | NASA Technical NotePublication details: Washington, D. C. National Aeronautics and Space Administration 1969Description: 43pSubject(s):
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Bound vol. contains NASA TN D 5371-5380

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