AIAA/DGLR Fifth International Aerospace Planes and Hypersonics Technologies Conference: 93-5100 - 93-5169

AIAA/DGLR Fifth International Aerospace Planes and Hypersonics Technologies Conference: 93-5100 - 93-5169

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Thrust characteristic comparison of turbojet (TJ), air-turborocket (ATR), pre- cooled turbojet (Pc TJ), turbofan (TF) and ramjet (RJ) engines The design point of all jet engine types is close to the minimum difference between thrust and drag.


Title:AIAA/DGLR Fifth International Aerospace Planes and Hypersonics Technologies Conference: 93-5100 - 93-5169
Author:
Publisher: - 1993
ISBN-13:

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