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Rapid supersonic performance prediction for 2D ramjet inlets

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Title of Paper:Rapid supersonic performance prediction for 2D ramjet inlets

Journal:Aerospace Science & Technology

Indexed by:Journal paper

Translation or Not:no

Co-author:Yan Ge,Hao Chen,Yu-fen Wen,Sheng-min Guo

Correspondence Author:Wen-zhong Xie

Pre One:Flow-Based Prediction for Self-Starting Limit of Two-Dimensional Hypersonic Inlets

Next One:A Ventral Diverterless High Offset S-shaped Inlet at Transonic Speeds
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