230 results on '"Uchiumi, Masaharu"'
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2. Investigation of Transition Phenomenon from Rotating Cavitation to Attached Asymmetric Cavitation by Coupled Analysis of One-Dimensional Flow Path Model of 3-Blade Inducer and Shaft Vibration System
3. Overspeeding characteristics of turbomachinery for gas generator cycle air turbo ramjet engine
4. Investigation of Transition Phenomenon from Rotating Cavitation to Attached Asymmetric Cavitation by Coupled Analysis of One-Dimensional Flow Path Model of 3-Blade Inducer and Shaft Vibration System
5. Flight Demonstration Experiment of Liquid Propellant Detonation Engine System Using Sounding Rocket S-520-34
6. Effect of Phase Transformation on Damping Performance of Wire Mesh Damper Made of Ni-Ti Shape Memory Alloy
7. Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31 in Space
8. OpenFOAMを用いたすべり軸受の振動特性評価手法の構築
9. Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31
10. 自己加圧式ハイブリッドロケットの推力一定制御
11. The Study on High-Precision Flow Rate Prediction for LOX/Ethanol Gas Generator
12. Combustion chamber temperature distribution of Gas Generator for GG-ATR engine
13. 観測ロケットS-520 31号機プロジェクト デトネーションエンジンシステムの宇宙動作実証結果
14. Flight Demonstration Experiment of Liquid Propellant Detonation Engine System Using Sounding Rocket S-520
15. Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket
16. Development of Visualization System for Fuel Regression of Paraffin Wax in Acceleration Environments
17. PID Throttle Control of Self-pressurized Hybrid Rocket Engine
18. Surface Temperature Distribution of LOX/LH2 Gas Generator for ATRIUM Engine
19. Throttling Fire Test of a LOX/Ethanol Gas Generator for the GG-ATR Engine
20. S-520-31号機によるデトネーションエンジンシステムの宇宙実験 －設計・試験・運用の概要－
21. S-520-31号機によるデトネーションエンジンシステムの宇宙実験 －実験結果報告とサクセスクライテリア評価－
22. ロケットスレッド実験におけるシステムインターフェース
23. ATRIUMエンジンの研究開発状況
24. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude
25. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: History from Development to Flight
26. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine
27. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: System Design
28. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Pulse Detonation Engine
29. Aeroacoustics of Hybrid Rockets
30. Space Flight Demonstration of Detonation Kick Motor Using Sounding Rocket S-520
31. 観測ロケット S-520 31号機プロジェクト：デトネーションエンジンシステムの宇宙実証
32. 18th International Symposium On Transport Phenomena and Dynamics of Rotating Machinery (isromac18)
33. Experimental Study On Temperature Change by Cavitation Accompanying Self-Pressurization of Propellant for Small Rocket Engines
34. 静止したハイブリッドロケットの音響放射特性
35. S-520-31号機によるデトネーションエンジン実験の進捗状況：デトネーションエンジンシステム
36. 推力10kN級エアターボロケットATRIUMエンジンの試作研究
37. S-520-31号機によるデトネーションエンジン実験の進捗状況：パルスデトネーションエンジン
38. ガス推進剤ブローダウン時の排出流量予測
39. Progress Status of a Detonation Engine System for Sounding Rocket S-520 No. 31: Rotating Detonation Engine
40. Supervised Learning for Generating Fair Curves with Curvature Boundary Conditions
41. Rotordynamic forces acting on three-bladed inducer under supersynchronous/synchronous rotating cavitation
42. Micro space propulsion unit in f3 engineering center
43. Prediction of liquid oxygen flow rate and experimental verification during throttling
44. The innovative aircraft unit in f3 center of Hokkaido univ. and Muroran IT
45. Development of Void Fraction Meter for Measuring Gas-liquid Two-phase Flow of Rocket Propellants
46. Suppression of cavitation instabilities in an inducer by J Groove
47. Experimental Study of the effect of Injector Orifice on Propulsive Performance of Rotating Detonation Engine
48. LOX/エタノールガスジェネレーターの温度場評価
49. 再使用型宇宙輸送システムにおける大気アシスト飛行の実証研究WGの活動状況
50. エアブリーザーによる垂直離着陸飛行実証計画
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