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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

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Abstract:

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

Relators: Dario Giuseppe Pastrone
Academic year: 2017/18
Publication type: Electronic
Number of Pages: 147
Subjects:
Corso di laurea: Corso di laurea magistrale in Ingegneria Aerospaziale
Classe di laurea: New organization > Master science > LM-20 - AEROSPATIAL AND ASTRONAUTIC ENGINEERING
Ente in cotutela: TUM - technische universit√§t m√ľnchen (GERMANIA)
Aziende collaboratrici: UNSPECIFIED
URI: http://webthesis.biblio.polito.it/id/eprint/6875
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