Title: Altitude Evaluation of Several Afterburner Design Variables on a J47-GE-17 Turbojet Engine
Abstract: From Introduction: 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.
Publication Year: 1953
Publication Date: 1953-10-23
Language: en
Type: article
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