Method for Rapid Graphical Evaluation of Cooled or Uncooled Turbojet and Turboprop Engine or Component Performance (effects of Variable Specific Heat Included) (1955)
NASA Technical Reports Server (NTRS) · leaf 42
3457 … Burner-inlet equivalent temperature, 0^ or 0^ Figure 6. - Primary-burner and afterburner fuel-air ratio. (A large working copy of this chart may be obtained by using the request card bound in the back of the report.) H
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
