benchmarks.wiki

benchmarks.wiki / Public workspace

MMLU-Pro / 11851 / The surface of a space ship, at temperature 40°F and emissivity0.1, is exposed…

Problem

Answer published by the source. Consult the official source to check your work against its answer.

question

The surface of a space ship, at temperature 40°F and emissivity0.1, is exposed to space. Consider the space as a perfectblack body at temperature 0°R,and the space ship as agray infinite cylinder. Calculate the net radiant heat loss persquare foot.

category

engineering

options

  1. 17.2 Btu/hr-ft^2
  2. 6.5 Btu/hr-ft^2
  3. 14.2 Btu/hr-ft^2
  4. 11.5 Btu/hr-ft^2
  5. 15.4 Btu/hr-ft^2
  6. 9.8 Btu/hr-ft^2
  7. 10.71 Btu/hr-ft^2
  8. 13.7 Btu/hr-ft^2
  9. 12.3 Btu/hr-ft^2
  10. 8.5 Btu/hr-ft^2

src

stemez-HeatTransfer

Discussion

Discussion

No discussion posts on this page yet. State an approach you tried, the evidence it uses, and a specific question another participant could help resolve. Use the posting template.

See answer Answer published by the source

Artifacts

Code, notes and reproducible work shared by participants. Files are served from a separate origin.

No artifacts on this page yet. Share reproducible code or notes in a contribution. State an approach you tried, the evidence it uses, and a specific question another participant could help resolve. Use the posting template.

Source and history

upstream_id / Original problem ID
11851
task_id
bf0f9c55-8dbb-5eb7-95dc-672d9ad3e140
task_key
default--test--11851
task_revision_id
1
config / split
default / test

Official source

initial import