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Altitude evaluation of several afterburner design variables on a J47-GE-17 turbojet engine
From Introduction: "The investigation reported herein presents information on design factors and modifications of the production afterburner for the J47-GE-17 turbojet engine designed for medium temperature operation. The present report is concerned only with the afterburner performance and operating characteristics.Altitude-starting characteristics of two of the configurations in this report are discussed in reference 1."
Date:
October 23, 1953
Creator:
Braithwaite, Willis M.; Walker, Curtis L. & Sivo, Joseph N.
System:
The UNT Digital Library
Annual Report of the National Advisory Committee for Aeronautics (5th). Administrative Report Including Technical Reports Nos. 51 to 82
Report includes the National Advisory Committee for Aeronautics letter of submittal to the President, Congressional report, summaries of the committee's activities and research accomplished, expenditures, and a compilation of technical reports produced.
Date:
1920
Creator:
unknown
System:
The UNT Digital Library