MATSUO Kazuyasu | Graduate School of Engineering, Sciences, Kyushu University

スポンサーリンク

概要

関連著者

もっと見る

著作論文

Investigations of Mach Reflection of a Shock Wave : 4th Report, The Transition between Regular and Mach Reflections
Investigations of Mach Reflection of a Shock Wave : 3rd Report, Strength of a Reflected Shock Wave
Investigations of Mach Reflection of a Shock Wave : 2nd Report, Shape of a Reflected Shock Wave
Studies of Condensation Shock Waves : 2nd Report, Relation between Condensation Shock Wave and Condensation Zone
Investigations of Mach Reflection of a Shock Wave : Part 1,Configurations and Domains of Shock Reflection
Relation between Condensation and Thermal Choking in an Unsteady Subsonic Flow
Effects of Condensing Flow on an Oblique Shok Wave in a Supersonic Nozzle
Oscillations of Laval Nozzle Flow with Condensation : Part 2, On the Mechanism of Oscillations and their Amplitudes
Oscillations of Laval Nozzle Flow with Condensation : Part 1,On the Range of Oscillations and their Frequencies
Investigations of Transonic Ludwieg Tubes : 4th Report, Effects of Flow Mach Number in Supply Tube on Starting Process of Test Section
Investigations of Transonic Ludwieg Tubes : Part3 Effects of Plenum Exhaust System on Starting Process of Tunnel Test Section
Investigations of Transonic Ludwieg Tubes Part 2 Starting Process in the Case of a Downstream Valve
Investigation of Transonic Ludwieg Tubes Part I Starting Process in the Case of an Upstream Valve
Modified Diffusion Model of Pseudo-Shock Waves Considering Upstream Boundary Layers
Investigation of Supersonic Air Ejectors : Part 2,Effects of Throat-Area-Ratio on Ejector Performance
Investigation of Supersonic Air Ejectors : Part 1. Performance in the Case of Zero-Secondary Flow
Investigation of the Starting Process of a Supersonic Wind Tunnel
The Error in Measuring an Accelerated Flow Velocity by a Spark Tracer Method
Flow Unsteadiness by Weak Normal Shock Wave/Turbulent Boundary Layer Interaction in Internal Flow
Extension of the Steady Flow Duration of a Ludwieg Tube Using a Reservoir-orifice Method : Part11, Case of Orifices with Variable Opening Area
Post-Shock Expansion Phenomenon Caused by Normal Shock/Turbulent Boundary Layer Interaction
Self-excited Oscillations of Supersonic Flow in a Sudden Enlargement of a Duct
Pseudo-Shock Waves in a Divergent Channel

もっと見る

スポンサーリンク