Attenuation of tangent-pressure oscillation in liquid-oxygen-heptane rocket engine combustion chamber using longitudinal fin
ATTENUATION OF TANGENTIAL-PRESSURE OSCILLATIONS IN A LIQUID-OXYGEN -N-HEPTANE ROCKET ENGINE WITH LONGITUDINAL FINS
1956-06-28
Sonstige
Keine Angabe
Englisch
Acoustic Streaming Effects in Liquid Rocket Engines with Tangential Mode Oscillations AIAA Paper
British Library Conference Proceedings | 2007
|Engineering Index Backfile | 1959
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