Computational Analysis of the Unsteady Flow Induced by a Projectile Overtaking a Preceding Shock Wave

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概要

• 論文の詳細を見る
• Japan Society for Aeronautical and Space Sciencesの論文
• 1998-08-04

著者

• FUJII Kozo

  The Institute of Space and Astronautical Science

• Watanabe Rikio

  Tokyo Noko University

• HIGASHINO Fumio

  Tokyo Noko University

• WATANABE Rikio

  Tokyo City University, Department of Mechanical Systems Engineering

関連論文

• Computational Analysis of the Flow Field Near the Boat-tail Region of Annular Plug Nozzles
• Preprocessed Visualization of Large Scale Unsteady Flow Simulations
• Flow Field and Performance Analysis of an Annular-Type Aerospike Nozzle with Base Bleeding
• Computational Analysis of the Unsteady Flow Induced by a Projectile Overtaking a Preceding Shock Wave
• Computers and Flow Visualization
• Thrust Performance Improvement for a Water/Liquid Nitrogen Rocket Engine

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