EXAMINATION OF THE EFFECT OF VISCOUS MODEL ON THRUST OF LIQUID OXYGEN / PARAFFIN FUELED HYBRID ROCKET ENGINE BY USING NUMERICAL METHOD | AVESİS

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EXAMINATION OF THE EFFECT OF VISCOUS MODEL ON THRUST OF LIQUID OXYGEN / PARAFFIN FUELED HYBRID ROCKET ENGINE BY USING NUMERICAL METHOD

Koçak D. , Özdamar A.

INTERNATIONAL ASIAN CONGRESS ON CONTEMPORARY SCIENCES-V, Nakhchivan, Azerbaijan, 1 - 02 June 2021, pp.1180-1186

Publication Type: Conference Paper / Full Text
City: Nakhchivan
Country: Azerbaijan
Page Numbers: pp.1180-1186