Publikationsdatum:
2019-07-13
Beschreibung:
Stress and vibration analysis of rocket engine turboprop inducer blades, using finite element method
Schlagwort(e):
PROPULSION SYSTEMS
Materialart:
AIAA PAPER 70-630
,
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH; Jun 15, 1970 - Jun 19, 1970; SAN DIEGO, CA
Format:
text
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