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Numerical analysis of contrail formation process and climate impact by aviation-induced cirrus by emissions from aircraft with alternative aviation fuels

JAXA Supercomputer System Annual Report February 2024-January 2025

Report Number: R24EDA201C35

Subject Category: Aeronautical Technology

PDF available here

  • Responsible Representative: Atsushi Kanda, Aviation Technology Directorate, Aviation Environmental Sustainability Innovation Hub
  • Contact Information: Keiichi Okai, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub(okai.keiichi@jaxa.jp)
  • Members: Keiichi Okai, Takuma Tadokoro, Ryo Yoshida

Abstract

In recent years, carbon neutrality has been declared in the aviation sector. As one of the greenhouse effects of aircraft exhaust gas, persistent contrail and contrail cirrus formation have been recognized as quite important most recently due to its expected large effects in radiative forcing. The present study investigates the effects of fuel characteristics of the major alternative aviation fuels (SAF and hydrogen) on the radiative forcing of contrails using a global climate model.

Reference URL

N/A

Reasons and benefits of using JAXA Supercomputer System

The global atmospheric calculations with additional contrail microphysics model require large computational resources.

Achievements of the Year

Based on the distribution data of the water vapor emission of simulated flight missions, the vertically averaged distribution of water vapor emission for jet-fuel aircraft is described as seen in Fig. 1.

Figure 2 shows the distribution of contrail radiative forcing for kerosene aircraft obtained by one-year simulation. The contrail radiative forcing for jet-fueled aircraft was estimated to be 67mW/m2, which is consistent with the available literature. Trials on the application of alternative fuel effects were investigated.

Annual Report Figures for 2024

Fig.1: Aggregated H2O emissions in kg/kg/s: zonal average at p = 193 hPa for jet-fueled aircraft.

 

Annual Report Figures for 2024

Fig.2: The distribution of contrail radiative forcing for Jet-fueled aircraft.

 

Publications

N/A

Usage of JSS

Computational Information

  • Process Parallelization Methods: MPI
  • Thread Parallelization Methods: N/A
  • Number of Processes: 720
  • Elapsed Time per Case: 11 Hour(s)

JSS3 Resources Used

 

Fraction of Usage in Total Resources*1(%): 0.00

 

Details

Please refer to System Configuration of JSS3 for the system configuration and major specifications of JSS3.

Computational Resources
System Name CPU Resources Used
(Core x Hours)
Fraction of Usage*2(%)
TOKI-SORA 0.00 0.00
TOKI-ST 0.00 0.00
TOKI-GP 0.00 0.00
TOKI-XM 0.00 0.00
TOKI-LM 0.00 0.00
TOKI-TST 0.00 0.00
TOKI-TGP 0.00 0.00
TOKI-TLM 0.00 0.00

 

File System Resources
File System Name Storage Assigned
(GiB)
Fraction of Usage*2(%)
/home 1759.00 1.19
/data and /data2 148330.00 0.71
/ssd 38250.00 2.05

 

Archiver Resources
Archiver Name Storage Used
(TiB)
Fraction of Usage*2(%)
J-SPACE 0.29 0.00

*1: Fraction of Usage in Total Resources: Weighted average of three resource types (Computing, File System, and Archiver).

*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.

 

ISV Software Licenses Used

ISV Software Licenses Resources
ISV Software Licenses Used
(Hours)
Fraction of Usage*2(%)
ISV Software Licenses
(Total)
0.00 0.00

*2: Fraction of Usage:Percentage of usage relative to each resource used in one year.

JAXA Supercomputer System Annual Report February 2024-January 2025