Oscillation Phenomena of Pseudo-Shock Waves
スポンサーリンク
概要
- 論文の詳細を見る
In the previous paper, we presented the diffusion model of pseudo-shock waves, by which the time-mean static pressure distributions in pseudo-shocks could be explained. In the actual flow, however, the pseudo-shock wave is not steady, but oscillates about a mean position and causes the fluctuations of the local static pressures. In this paper the oscillation phenomena of pseudo-shocks in a straight pipe were experimentally investigated and the causes and the frequencies of oscillations were discussed. As the results, it was found that the oscillation of the pseudo-shock became stronger with the increasing Mach number and the maximum wall static pressure fluctuation induced by the oscillation amounted to about 60 per cent of the difference of static pressures before and behind the shock. Moreover, it was showed that this oscillating phenomena could be explained by the interaction of the shock with the small disturbances existing in the supersonic flow upstream the shock.
- 一般社団法人日本機械学会の論文
著者
-
Nagai Minoru
Faculty Of Engineering And Science Ryukyu University
-
Ikui Takefumi
Faculty Of Engineering Kyushu University
-
Matsuo Kazuyasu
Faculty Of Engineering Kyushu University
-
HONJO Masanobu
Kobe Technical Institute, Mitsubishi Heavy Industries Ltd.
-
Honjo Masanobu
Kobe Technical Institute Mitsubishi Heavy Industries Ltd.
-
MATSUO Kazuyasu
Faculty of Engineering, Kyushu University
関連論文
- 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
- Mechanism of Pseudo-shock Wave in Supersonic Jet
- Extension of the Steady Flow Duration of a Ludwieg Tube Using a Reservoir-Orifice Method : Part 1. Case of Orifices with Fixed Opening Area
- Modified Diffusion Model of Pseudo-Shock Waves Considering Upstream Boundary Layers
- Choking Phenomena of Flows in a Shock Tube
- The Interaction of a Reflected Shock Wave with the Contact Region in a Shock Tube
- The Interaction of a Reflected Shock Wave with the Boundary Layer in a Shock Tube
- Investigations of the Aerodynamic Characteristics of the Shock Tubes : Part 3 Transient Flow in Converging-Diverging Nozzles
- Oscillation Phenomena of Pseudo-Shock Waves
- The Mechanism of Pseudo-Shock Waves
- Investigations of the Aerodynamic Characteristics of the Shock Tubes : (Part 2,On the Formation of Shock Waves)
- Fast-Acting Valves for Use in Shock Tubes : Part 2, Formation of shock waves
- Fast-Acting Valves for Use in Shock Tubes : Part 1, Construction and their characteristics
- Investigations of the Aerodynamic Characteristics of the Shock Tubes : (Part 1,The Effects of Tube Diameter on the Tube Performance)
- Investigations of the Aerodynamic Characteristics of the Shock Tubes : Part 4, Aerodynamic Characteristics of Laval Nozzles Installed in a Shock Tube
- Self-excited Oscillations of Supersonic Flow in a Sudden Enlargement of a Duct
- Pseudo-Shock Waves in a Divergent Channel
- RESEARCHES ON THE TWO-DIMENSIONAL CASCADE : Part 5,On the Performance of Flat-Plate Cascade
- Predicting Equivalent Performance of Blowers and Compressors for Gases from Air Test Data : Some Problems Encountered in the Translation of Compressor Performance
- A DESIGN OF AXIAL-FLOW COMPRESSOR BLADES WITH INCLINED STREAM SURFACE AND VARYING AXIAL VELOCITY
- EFFECT OF BLADE THICKNESS ON THE TWO-DIMENSIONAL CASCADE PERFORMANCE : Correcting Method for Design Camber and Stagger
- Measurement of Three Dimensional Flow Field behind on Impeller by Means of Periodic Multi-sampling with a Slanted Hot Wire
- Researches on the Two-Dimensional Retarded Cascade : Part 4,Determination of Blade Elements at Retarded Blade Row
- Researches on the Two-Dimensional Retarded Cascade : Part 3,Cascade Performances at High Inlet Angles
- Researches on the Two-Dimensional Retarded Cascade : Part 2, Method of the Cascade Testing
- Researches on the Two-Dimensional Retarded Cascade : Part 1, Contraction Effect in the Cascade
- Operating Characteristics of DC Arc Plasma Torch : I. Operation at Atmospheric Pressure Using Argon Gas
- Predicting Equivalent Performance of Gas Blowers and Compressors from Air Test Data : Present State and Prospective Subject