naca-rm-e9l02 Altitude Wind Tunnel Investigation of Combusiton Chamber Performance on J47 Turbojet Engine.pdfDownload 

National Advisory Committee for Aeronautics, Research Memorandum - Altitude Wind Tunnel Investigation of Combustion Chamber Performance on J47 Turbojet Engine

Have A Comment On This Article? Post It Here.

Comments are moderated and will not be published until approved. Your email address will be kept confidential. Please review our Comment Policy before posting your comment.