Personal profile

Disciplinary Calssification

ING-IND/07

Fingerprint Fingerprint is based on mining the text of the persons scientific documents to create an index of weighted terms, which defines the key subjects of each individual researcher.

  • 6 Similar Profiles
Coolants Engineering & Materials Science
Cooling Engineering & Materials Science
Heat transfer Engineering & Materials Science
Methane Engineering & Materials Science
Rocket engines Engineering & Materials Science
coolants Physics & Astronomy
cooling Physics & Astronomy
Temperature Engineering & Materials Science

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Research Output 2007 2016

  • 311 Citations
  • 10 h-Index
  • 14 Article
  • 13 Conference contribution
4 Citations

A CFD-derived correlation for methane heat transfer deterioration

Pizzarelli, M. 1 Feb 2016 In : Numerical Heat Transfer; Part A: Applications. 69, 3, p. 242-264 23 p.

Research output: Contribution to journalArticle

methane
Methane
Heat transfer
deterioration
heat transfer
4 Citations

Experimental investigation of transcritical methane flow in rocket engine cooling channel

Votta, R., Battista, F., Salvatore, V., Pizzarelli, M., Leccese, G., Nasuti, F. & Meyer, S. 25 May 2016 In : Applied Thermal Engineering. 101, p. 61-70 10 p.

Research output: Contribution to journalArticle

Methane
Cooling
Rocket engines
Temperature
Flow rate
1 Citations

Validation of conjugate heat transfer model for rocket cooling with supercritical methane

Pizzarelli, M., Nasuti, F., Votta, R. & Battista, F. 2016 In : Journal of Propulsion and Power. 32, 3, p. 726-733 8 p.

Research output: Contribution to journalArticle

heat transfer
Heat transfer
coolants
Coolants
methane

Assessment of a conjugate heat transfer model for rocket engine cooling channels fed with supercritical methane

Pizzarelli, M., Nasuti, F., Votta, R. & Battista, F. 2015 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc, AIAA

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Coolants
Heat transfer
Rocket engines
Methane
Cooling
10 Citations

Heat transfer modeling for supercritical methane flowing in rocket engine cooling channels

Pizzarelli, M., Nasuti, F., Onofri, M., Roncioni, P., Votta, R. & Battista, F. 22 Jan 2015 In : Applied Thermal Engineering. 75, p. 600-607 8 p.

Research output: Contribution to journalArticle

Heat transfer
Coolants
Methane
Rocket engines
Surface roughness