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
28.06.1956
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
|Liquid Oxygen/Liquid Methane Rocket Engine Development
British Library Conference Proceedings | 2007
|