35 results on '"Sato, Kazuo"'
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2. Aerodynamic Characteristics of Lifting Body HYFLEX under High-Temperature Real-Gas Conditio
3. Basic characteristics of the free-piston driven expansion tube JAXA HEK-X
4. Porous Injection Effect on Surface Heat Flux in High-enthalpy High-Reynolds number flow
5. Free-flight aerodynamic test with projectile-onboard data recorder in a ballistic range
6. Heat Flux Anomaly In High-Enthalpy And High-Reynolds Number Flow
7. Measurement of surface pressure fluctuation in hypersonic high-enthalpy boundary layer on a 7-degree cone model
8. Free-flight aerodynamic test of elliptic cone in Shock Tunnel
9. Miniature Data-Logger for Aerodynamic Force Measurement in Impulsive Facility
10. Aeroheating measurements on a reentry capsule model in free-piston shock tunnel HIEST
11. Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST
12. Free-flight aerodynamic tests of reentry vehicles in high-temperature real-gas flow (Invited)
13. Aeroheating measurement of Apollo shaped capsule with boundary layer trip in the free-piston shock tunnel HIEST
14. Free-flight tests of reentry capsule models in free-piston shock tunnel
15. Free-flight aerodynamic test with projectile-onboard data recorder in a ballistic range
16. Free-flight force measurement technique in shock tunnel
17. Measurement of surface pressure fluctuation in hypersonic high-enthalpy boundary layer on a 7-degree cone model
18. Miniature Data-Logger for Aerodynamic Force Measurement in Impulsive Facility
19. Measurement of hypersonic high-enthalpy boundary layer transition on a 7º cone model
20. Heat flux measurement of Apollo capsule model in the free-piston shock tunnel HIEST
21. Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-off Distance
22. Influence of Thermal Non-equilibrium on Nozzle Flow Condition of High Enthalpy Shock Tunnel HIEST
23. Measurement of Hypersonic Boundary Layer Transition on Cone Models in the Free-Piston Shock Tunnel HIEST
24. Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight
25. Aerodynamic characteristics of generic models under real-gas condition in the free-piston shock tunnel HIEST
26. Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST
27. Performance Characteristics of Scramjet Engine with Different Combustor Shapes at Hypervelocity Condition over Mach 10 Flight
28. Effect of Combustor Shape on Scramjet Characteristics at Hypervelocity Condition over Mach 10 Flight
29. Laser Absorption Spectroscopy for Determination of Flow Characteristics in High Enthalpy Shock Tunnel
30. Numerical Analysis of Experimental Results on the Surface Catalycity in HIEST
31. Viscous Drag Reduction in a Mach 12 Scramjet Engine
32. Experimental study on flow establishment in a large scale scramjet
33. Development of a new force measurement method for scramjet testing in a high enthalpy shock tunnel
34. Hypervelocity aerothermodynamic and propulsion research using a high enthalpy shock tunnel HIEST
35. Ignition strategy in a model scramjet
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