Inverse heat conduction method and heat flux error estimation in rocket engines

Cosimo Ciraci'

Inverse heat conduction method and heat flux error estimation in rocket engines.

Rel. Dario Giuseppe Pastrone. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2018

Preview

PDF (Tesi_di_laurea) - Tesi
Licenza: Creative Commons Attribution Non-commercial No Derivatives.
Download (5MB) | Preview

Investigation of transient start-up behaviour in an Oxygen/Methane rocket combustion chamber.

Elettronica

Modifica (riservato agli operatori)