Carmine Carmicino - Publications, H-index & Citations

Carmine Carmicino

University of Naples Federico II

16H指数

62论文数

1.1K被引数

收录论文 8

发表时间

Prediction of the fuel regression-rate in a HDPE single port hybrid rocket fed by liquid nitrous oxide

COMBUSTION AND FLAME

IF6.2

2024-01-01

PREAI

Gallo, Giuseppe; Kamps, Landon; Hirai, Shota; Carmicino, Carmine; Harunori, Nagata

One-dimensional modelling of the nozzle cooling with cryogenic oxygen flowing through helical channels in a hybrid rocket

ACTA ASTRONAUTICA

IF3.4

2023-09-01

PREAI

Gallo, Giuseppe; Kamps, Landon; Hirai, Shota; Carmicino, Carmine; Nagata, Harunori

Self-consistent surface-temperature boundary condition for liquefying-fuel-based hybrid rockets internal-ballistics simulation

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER

IF5.8

2021-04-01

PREAI

Carmicino, Carmine; Gallo, Giuseppe; Savino, Raffaele

Computational fluid-dynamic modeling of the internal ballistics of paraffin-fueled hybrid rocket

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2019-06-01

PREAI

Di Martino, G. D.; Mungiguerra, S.; Carmicino, C.; Savino, R.

Analytical modeling of the one-dimensional acoustic field in hybrid rocket combustion chamber

JOURNAL OF SOUND AND VIBRATION

IF4.9

2018-12-01

PREAI

Carmicino, Carmine; Di Martino, Giuseppe D.

A simplified computational fluid-dynamic approach to the oxidizer injector design in hybrid rockets

ACTA ASTRONAUTICA

IF3.4

2016-12-01

PREAI

Di Martino, Giuseppe D.; Malgieri, Paolo; Carmicino, Carmine; Savino, Raffaele

Trade-off between paraffin-based and aluminium-loaded HTPB fuels to improve performance of hybrid rocket fed with N2O

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2014-08-01

PREAI

Carmicino, C.; Scaramuzzino, F.; Sorge, A. Russo

Performance comparison between two different injector configurations in a hybrid rocket

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2007-01-01

PREAI

Carmicino, C.; Sorge, A. Russo

研究方向