EFFECT OF NOZZLE SHAPES ON THE PERFORMANCE OF CONTINUOUSLY-ROTATING DETONATION ENGINE
48th, Aerospace sciences meeting; 48th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition ; 2010 ; Orlando, FL
2010-01-01
8 pages
Includes bibliographical references and index; Also contains papers from the New Horizons Forum and Aerospace Exhibit 2009
Conference paper
English
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Propulsive Performance of a Continuously Rotating Detonation Engine
Online Contents | 2011
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