Modeling gas turbine cycles improves the design of turbofan engines by assessing mixing processes.
A simplified model of the mixing process in turbo-fan engines is examined, and while qualitatively useful this is found to have serious shortcomings. A more rigorous approach, using the N.R.C. Jet Engine Design Point computer program is presented, and a design procedure working to a limiting tailpipe area is suggested.
No takes yet. Share an insight, caveat, or question.
E.P. Cockshutt (1964) studied this question.
Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context: