Kapak Resmi

Finite element analysis for rocket motor case under internal pressure and thermal loads / M. A. Muhammad ... [et al.]

Rocket motor combustion chamber needs to contain very high pressure and temperature due to burning of rocket fuels. For that reason, the combustion chamber is required to withstand the stresses caused by the static and thermal load generated by the burning of the rocket fuels. History demonstrated t...

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Detaylı Bibliyografya
Asıl Yazarlar:	Muhammad, M. A. (Yazar), Salleh, Z. (Yazar), Hamid, A. H. A. (Yazar), Sujana, M. J. (Yazar), Kamaludin, K. (Yazar)
Materyal Türü:	Kitap
Baskı/Yayın Bilgisi:	Smart Manufacturing Research Institute (SMRI), 2022-09.
Konular:	Article PeerReviewed
Online Erişim:	Link Metadata
Etiketler:	Etiketle Etiket eklenmemiş, İlk siz ekleyin!

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