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

Bildiriler > Tam Metin Bildiri · 2021

Yazarlar: Dilara KOÇAK, Aydoğan ÖZDAMAR

INTERNATIONAL ASIAN CONGRESS ON CONTEMPORARY SCIENCES-V, Azerbaycan, Uluslararası, Sözlü Sunum, Tam Metin Bildiri, 2021-2021, ss 1180-1186

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