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 45
44 NACA TN 3335 Figure 9. - Specific thrust for convergent-divergent exhaust nozzle. (A large working copy of this chart may he obtained by usln^ the request card bound in the back of the report.)
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
