Weight-flow and thrust limitations due to use of rotating combustors in a turbojet engine

Author: Lezberg, Erwin A.
Additional Authors: Blackshear, Perry L., Jr.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E55K16
Link: https://digital.library.unt.edu/ark:/67531/metadc61872/

< New search