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47 results on '"Takeshi Kanda"'

3. Expander and Coolant-Bleed Cycles of Methane-Fueled Rocket Engines

Author

Hiroya Asakawa, Toshiya Kimura, Takeshi Kanda, and Masaki Sato

Subjects
020301 aerospace & aeronautics, business.product_category, Materials science, business.industry, Nuclear engineering, Aerospace Engineering, 02 engineering and technology, Bleed, 01 natural sciences, Methane, 010305 fluids & plasmas, Coolant, chemistry.chemical_compound, 0203 mechanical engineering, chemistry, Rocket, Space and Planetary Science, 0103 physical sciences, Rocket engine, business
Published
2018
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5. Experimental Study of Heat Flux in the Pseudo-shock Region

Author

Kanenori Kato and Takeshi Kanda

Subjects
020301 aerospace & aeronautics, Materials science, Critical heat flux, Aerospace Engineering, 02 engineering and technology, Heat transfer coefficient, Mechanics, Heat Flux, 01 natural sciences, 010305 fluids & plasmas, Shock (mechanics), 0203 mechanical engineering, Heat flux, Space and Planetary Science, 0103 physical sciences, Pseudo-shock, Nucleate boiling
Abstract

形態: 図版あり, Physical characteristics: Original contains illustrations, Accepted: 2016-04-12, 資料番号: PA1710084000

Published
2016

6. Extended Tsiolkovskii Equation and Its Application to Launch Vehicles

Author

Takeshi Kanda, Kouichi Takasaki, and Kouichiro Tani

Subjects
Lift coefficient, Engineering, business.industry, Angle of attack, 020209 energy, Aerospace Engineering, 02 engineering and technology, Impulse (physics), Mass ratio, Space and Planetary Science, Drag, 0202 electrical engineering, electronic engineering, information engineering, Specific impulse, Scramjet, Aerospace engineering, business, Ramjet
Abstract

形態: 図版あり, Physical characteristics: Original contains illustrations, Accepted: 2016-06-11, 資料番号: PA1710041000

Published
2016

7. Conceptual Design Model of High-Altitude Test Stand for Rocket Engines

Author

Takeshi Kanda, Daizo Sugimori, Yohei Ogawa, and Makoto Kojima

Subjects
Engineering, business.product_category, Condensation, Rocket engine nozzle, Aerospace Engineering, Rocket Engine, 02 engineering and technology, law.invention, 0203 mechanical engineering, Aeronautics, Conceptual design, law, Ejector, Aerospace engineering, 020301 aerospace & aeronautics, business.industry, Diffuser, Injector, Effects of high altitude on humans, Saturation, Test (assessment), 020303 mechanical engineering & transports, HATS, Rocket, Space and Planetary Science, Rocket engine, business
Abstract

Conceptual design procedures and design models of HATS are revised and renewed. The results calculated using the revised method are compared with the operating conditions of HATS at the JAXA Kakuda Space Center. The previous physical method of test chamber pressure and that of ejector suction are adopted in the present model. The suction model adopts the inviscid momentum exchange mechanism. The deceleration process in the supersonic diffuser is revised using the pseudo-shock model. Physical and thermodynamic models are constructed for condensation and steam saturated flow conditions. The results calculated are in reasonable agreement with the measured values (e.g., pressure of secondary flow at the ejector section and pressure changes during engine shut down). The effect of ejector steam condensation on the operating conditions of HATS is quantitatively presented., 形態: 図版あり, Physical characteristics: Original contains illustrations, 資料番号: PA1610066000

Published
2016

8. Conservation-Law Approach for Transition in Pipe Flows

Author

Takeshi Kanda

Subjects
Conservation law, Engineering, Momentum, Operations research, business.industry, Turbulence, Aerospace Engineering, Laminar flow, Conservation, Mechanics, 01 natural sciences, 010305 fluids & plasmas, Pipe flow, Laminar Flow, Space and Planetary Science, Transition, 0103 physical sciences, Turbulent Flow, 010306 general physics, business, Pipe Flow
Abstract

形態: 図版あり, Physical characteristics: Original contains illustrations, Accepted: 2016-07-20, 資料番号: PA1710080000

Published
2016
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9. Analytical Method for Prediction of Suction Performance of Ejector-Jet

Author

Takeshi Kanda, Shuichi Ueda, Kouichiro Tani, Harunori Nagata, and Susumu Hasegawa

Subjects
Jet (fluid), Suction, Materials science, Space and Planetary Science, law, Ejector-jet, Aerospace Engineering, Thermodynamics, Air-breathing Engine, Combined Cycle, Injector, Mechanics, law.invention
Abstract

To reduce the cost of space transportation, air-breathing engines are considered to be candidates for propulsion. However, to cover a wide range of flight speeds, the propulsion system has to operate in various modes to be efficient under incoming atmospheric-air conditions. The Japan Aerospace Exploration Agency is proposing a rocket-based combined cycle engine for operation under various condition, an ejector-jet mode being adopted for the low-speed regime. The suction performance ejector-jets has long been studied experimentally and numerically at JAXA, and little success has been achieved in explaining the deterioration of suction performance with high-temperature gas or light gas such as helium. In the present study, based on former models, a simple one-dimensional model was introduced incorporating the mixing effects of the primary flow (rocket flow) and secondary flow (induced air flow). The results were compared using several experimental and numerical data to check the plausibility of the model. It was found that if greater mixing occurs, suction performance is degraded, explaining the actual phenomena of the experiments., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: PA1610077000

Published
2015
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10. ロケットエンジンターボポンプのスロットリング作動について

Author

Takeshi Kanda

Subjects
Engineering, Injection, business.industry, Aerospace Engineering, Rocket Engine, Bandwidth throttling, Conceptual study, Circulation, Throttling, Aeronautics, Space and Planetary Science, Rocket engine, Aerospace engineering, business, Turbopump
Abstract

The 43rt JSASS Annual Meeting (April 12-13, 2012. Sanjo Conference Hall, The University of Tokyo), Tokyo, Japan, 資料番号: PA1210039000

Published
2013

12. Conservation-Law Approach to Prediction of Boundary Layer Transition

Author

Takeshi Kanda

Subjects
Mach number, unit Reynolds number, transition, Aerospace Engineering, Reynolds number, Magnetic Reynolds number, Mechanics, Boundary layer thickness, Reynolds equation, Physics::Fluid Dynamics, Flow separation, symbols.namesake, Boundary layer, Transition point, Space and Planetary Science, bluntness, symbols, Statistical physics, wall cooling, Reynolds-averaged Navier–Stokes equations, Mathematics
Abstract

2010 Asian Joint Conference on Propulsion and Power (March 4-6, 2010.), Miyazaki, Japan, 資料番号: AC1000137000, レポート番号: AJCPP2010-003

Published
2011
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13. Mach-8 Tests of a Combined-Cycle Engine Combustor

Author

Atsuo Murakami, Kanenori Kato, Kenji Kudo, and Takeshi Kanda

Subjects
Propellant, Materials science, Waste management, Mechanical Engineering, Airflow, Aerospace Engineering, Pitot tube, Injector, Mechanics, Fuel injection, Combustion, law.invention, Fuel Technology, Space and Planetary Science, law, Combustor, Combustion chamber
Abstract

著者人数: 4名, 資料番号: AC1000038000

Published
2007
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14. Suppression of Combustor-Inlet Interaction in a Scramjet Engine under Mach 4 Flight Conditions

Author

Kan Kobayashi, Noboru Sakuranaka, Tohru Mitani, Takeshi Kanda, Sadatake Tomioka, and Kouichiro Tani

Subjects
Engineering, geography, geography.geographical_feature_category, business.industry, Aerospace Engineering, Propulsion, Combustion, Inlet, symbols.namesake, Mach number, Space and Planetary Science, Combustor, symbols, Scramjet, Aerospace engineering, business, Scramjet engine
Abstract

資料番号: ARDS06125000

Published
2007
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15. Conceptual Study of a Rocket-Ramjet Combined-Cycle Engine for an Aerospace Plane

Author

Kouichiro Tani, Takeshi Kanda, and Kenji Kudo

Subjects
Engineering, Hypersonic speed, business.product_category, business.industry, Mechanical Engineering, Hypersonic flight, Aerospace Engineering, Thrust, Fuel Technology, Rocket, Space and Planetary Science, Scramjet, Supersonic speed, Specific impulse, Aerospace engineering, business, Ramjet
Abstract

著者人数: 3名, 資料番号: AC1000036000

Published
2007

16. Multidisciplinary Design Optimization of Space Plane Considering Rigid Body Characteristics

Author

Nobuhiro Yokoyama, Takeshi Kanda, Hideyuki Taguchi, Shinji Suzuki, and Takeshi Tsuchiya

Subjects
Engineering, business.industry, Payload, Multidisciplinary design optimization, Aerospace Engineering, Control engineering, Rigid body, Metamodeling, Nonlinear programming, Center of gravity, Space and Planetary Science, Multidisciplinary approach, Airframe, business
Abstract

DOI: 10.2514/1.19969 Multidisciplinary designoptimization isanimportant approachfor the conceptualdesignof space planesbecause these planes are characterized by disciplines that interact with one another. A multidisciplinary design optimization problemof asingle-stage-to-orbit space plane isformulated andsolved inthis study.Themodeling andoptimization ofrigidbodycharacteristics,suchastrimandstability,arefocusedonbecauseasingle-stage-to-orbitspaceplanehas a tendency for considerable shift of both the aerodynamic center and the center of gravity. Moreover, the design of the air-breathing engines are integrated with the airframe and its effect on the rigid body characteristics are also modeled in the framework of multidisciplinary design optimization. Using the all-at-once-based multidisciplinary design optimization approach, which incorporates sparse nonlinear programming and metamodeling, the design of the vehicle and its flight trajectory are successfully optimized. Finally, the characteristics of the optimal solution are investigated, especially the relationships among the airframe-engine integration, rigid body characteristics, and payload transportation capability.

Published
2007
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17. Downstream Ramjet-Mode Combustion in a Dual-Mode Scramjet Engine

Author

Takeshi Kanda, Kanenori Kato, Atsuo Murakami, Kan Kobayashi, and Kenji Kudo

Subjects
Materials science, business.industry, Mechanical Engineering, Aerospace Engineering, Pitot tube, Mechanics, Static pressure, Combustion, Fuel injection, law.invention, Fuel Technology, Space and Planetary Science, law, Combustor, Combustion chamber, Aerospace engineering, Total pressure, business, Ramjet
Abstract

著者人数: 5名, 資料番号: AC1000034000

Published
2006
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18. Experiments on a Scramjet Engine with Ramp-Compression Inlet at Mach 8

Author

Kan Kobayashi, Toshihito Saito, Takeshi Kanda, and Tetsuo Hiraiwa

Subjects
Engineering, business.industry, Mechanical Engineering, Airflow, Aerospace Engineering, Thrust, Static pressure, Fuel injection, Adverse pressure gradient, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, Drag, symbols, Combustor, Aerospace engineering, business
Abstract

著者人数: 4名, 資料番号: AC1000033000

Published
2006

19. Aerodynamic Performance of Scramjet Inlet Models with a Single Strut

Author

Kenji Kudou, Kouichiro Tani, and Takeshi Kanda

Subjects
Shock wave, Materials science, business.industry, Mechanical Engineering, Aerospace Engineering, Aerodynamics, Static pressure, Structural engineering, Mechanics, symbols.namesake, Flow separation, Fuel Technology, Mach number, Space and Planetary Science, symbols, Scramjet, Total pressure, business, Wind tunnel
Abstract

著者人数: 3名, 資料番号: AC1000035000

Published
2006

20. Performance of Supersonic Combustors with Fuel Injection in Diverging Section

Author

Sadatake Tomioka, Kan Kobayashi, Atsuo Murakami, Takeshi Kanda, and Kenji Kudo

Subjects
Engineering drawing, Materials science, Mechanical Engineering, Aerospace Engineering, Mechanics, Combustion, Fuel injection, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, Section (archaeology), symbols, Total air temperature, Combustor, Supersonic speed, Freestream, Wind tunnel
Abstract

著者人数: 5名, 資料番号: AC1000032000

Published
2006

21. Aerodynamic Experiment on an Ejector-Jet

Author

Kenji Kudo, Goro Masuya, Shigeki Aoki, Takeshi Kanda, and Jongsun Lee

Subjects
Materials science, Mass flow meter, Meteorology, Mechanical Engineering, Isothermal flow, Aerospace Engineering, Mechanics, Secondary flow, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, Prandtl–Meyer function, Total air temperature, Mass flow rate, symbols, Total pressure
Abstract

著者人数: 5名, 資料番号: AC1000031000

Published
2005

22. Staging of Two-Stage-to-Orbit Aerospace Plane

Author

Takeshi Kanda and Kenji Kudo

Subjects
Engineering, Staging, Unstart, business.industry, Plane (geometry), Shutdown, Trajectory, Aerospace Engineering, Aerospace Plane, Space and Planetary Science, Drag, Two-stage-to-orbit, Pitching moment, Pitching Moment, Aerospace engineering, Aerospace, business
Abstract

24th Congress of International Council of the Aeronautical Sciences (August 29-September 3, 2004.), Yokohama, Kanagawa, Japan, 資料番号: AC1000135000, レポート番号: ICAS 2004-1.11.1

Published
2005

23. Calculation of Dual-Mode Engine Performance

Author

Kanenori Kato, Kouichiro Tani, Kenji Kudo, and Takeshi Kanda

Subjects
Engineering, Space and Planetary Science, business.industry, Pseudo-Shock, Dual mode, Dual-mode engine, Aerospace Engineering, Ramjet, Scramjet, business, SSTO, Automotive engineering
Abstract

2005 Asian Joint Conference on Propulsion and Power (January 27-29, 2005.), Kitakyushu, Fukuoka, Japan, 資料番号: AC1000138000, レポート番号: AJCPP2005-22132

Published
2005

24. Dual-Mode Operations in a Scramjet Combustor

Author

Takeshi Kanda, Kenji Kudo, Nobuo Chinzei, and Atsuo Murakami

Subjects
Propellant, Materials science, business.industry, Mechanical Engineering, Dual mode, Aerospace Engineering, Fuel injection, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, Combustor, symbols, Scramjet, Aerospace engineering, business, Ramjet
Abstract

著者人数: 4名, 資料番号: AC1000029000

Published
2004
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25. Autoignited Combustion Testing in aWater-Cooled Scramjet Combustor

Author

Kenji Kudo, Takeshi Kanda, Nobuo Chinzei, Atsuo Murakami, and Tetsuo Hiraiwa

Subjects
Materials science, Waste management, Mechanical Engineering, Airflow, Aerospace Engineering, Autoignition temperature, Mechanics, Combustion, law.invention, Ignition system, Fuel Technology, Space and Planetary Science, law, Combustor, Total air temperature, Scramjet, Ignition timing
Abstract

著者人数: 5名, 資料番号: AC1000030000

Published
2004

26. Conceptual Study of a Combined-Cycle Engine for an Aerospace Plane

Author

Takeshi Kanda and Kenji Kudo

Subjects
Engineering, business.product_category, business.industry, Mechanical Engineering, Aerospace Engineering, Physics::Fluid Dynamics, symbols.namesake, Fuel Technology, Rocket, Mach number, Space and Planetary Science, Combustor, symbols, Scramjet, Pitching moment, Aerospace engineering, business, Engine coolant temperature sensor, Ramjet, Liquid hydrogen
Abstract

著者人数: 2名, 資料番号: AC1000027000

Published
2003

28. Effect of Integration of Scramjet into Airframe on Engine Performance and Payload

Author

Daisuke Akihisa, Goro Masuya, Kenji Kudo, Kouichiro Tani, and Takeshi Kanda

Subjects
geography, Engineering, Prandtl–Meyer expansion fan, geography.geographical_feature_category, business.industry, Mechanical Engineering, Nozzle, Aerospace Engineering, Thrust, Inlet, Fuel Technology, Space and Planetary Science, Drag, Airframe, Scramjet, Aerospace engineering, business, Wind tunnel
Abstract

著者人数: 5名, 資料番号: AC1000026000

Published
2002
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29. Mach 8 Testing of a Scramjet Engine with Ramp Compression

Author

Kan Kobayashi, Toshihito Saito, Kouichiro Tani, Tetsuji Sunami, and Takeshi Kanda

Subjects
Engineering, business.industry, Mechanical Engineering, Aerospace Engineering, Thrust, Combustion, Fuel injection, law.invention, Ignition system, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, law, Hydrogen fuel, symbols, Scramjet, Aerospace engineering, business, Ramjet
Abstract

著者人数: 5名, 資料番号: AC1000025000

Published
2002

30. Reaction and Mixing-Controlled Combustion in Scramjet Engines

Author

Tohru Mitani, Takeshi Kanda, and Nobuo Chinzei

Subjects
Materials science, Storage heater, Mechanical Engineering, Homogeneous charge compression ignition, Nuclear engineering, Mixing (process engineering), Aerospace Engineering, Combustion, Automotive engineering, symbols.namesake, Fuel Technology, Mach number, Internal combustion engine, Space and Planetary Science, Compression ratio, symbols, Combustor, Scramjet, Ignition timing, Engine knocking, Equivalence ratio
Abstract

AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 9th, Norfolk, VA, Nov. 1-5, 1999, 資料番号: AC1000062000, レポート番号: AIAA-1999-4871

Published
2001
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31. Effect of Sides-Spillage from Airframe on Scramjet Engine Performance

Author

Kouichiro Tani, Kenji Kudo, Daisuke Akihisa, and Takeshi Kanda

Subjects
geography, Engineering, geography.geographical_feature_category, business.industry, Plane (geometry), Mechanical Engineering, Aerospace Engineering, Thrust, Aerodynamics, Inlet, symbols.namesake, Spillage, Fuel Technology, Mach number, Space and Planetary Science, Airframe, symbols, Aerospace engineering, business, Marine engineering, Wind tunnel
Abstract

著者人数: 4名, 資料番号: AC1000023000

Published
2001

32. Mach 8 Testing of a Scramjet Engine Model

Author

Kouichiro Tani, Sadatake Tomioka, Tohru Mitani, Takeshi Kanda, and Tetsuji Sunami

Subjects
Materials science, Shock (fluid dynamics), Mechanical Engineering, Aerospace Engineering, Mechanics, Static pressure, Fuel injection, Combustion, law.invention, Ignition system, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, law, Combustor, symbols, Scramjet
Abstract

著者人数: 5名, 資料番号: AC1000022000

Published
2001
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33. Drags in Scramjet Engine Testing: Experimental and Computational Fluid Dynamics Studies

Author

Takeshi Kanda, Yasutaka Igarashi, Tohru Mitani, Tetsuo Hiraiwa, and Kazuhiro Nakahashi

Subjects
Engineering, Drag coefficient, business.industry, Mechanical Engineering, Aerospace Engineering, Computational fluid dynamics, law.invention, symbols.namesake, Fuel Technology, Pressure measurement, Mach number, Space and Planetary Science, Drag, law, Parasitic drag, symbols, Drag divergence Mach number, Aerospace engineering, business, Ramjet
Abstract

著者人数: 5名, 資料番号: AC1000021000

Published
1999

34. Airframe- Configuration Effect on Condition of Airflow to Engine in Hypersonic Flow

Author

Atsuo Murakami, Masatoshi Kodera, Takeshi Kanda, Kanenori Kato, and Kenji Kudo

Subjects
Lift-to-drag ratio, Hypersonic speed, Materials science, Angle of attack, business.industry, Mechanical Engineering, Airflow, Aerospace Engineering, Thrust, Aerodynamics, Fuel Technology, Space and Planetary Science, Airframe, Supersonic speed, Aerospace engineering, business
Abstract

著者人数: 5名, 資料番号: AC1000037000

Published
2007
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35. Comparison of Scramjet Engine Performance in Mach 6 Vitiated and Storage-Heated Air

Author

Tohru Mitani, Kouichiro Tani, Tetsuo Hiraiwa, Takeshi Kanda, Shigeru Sato, and Sadatake Tomioka

Subjects
Materials science, Mechanical Engineering, Storage heater, Aerospace Engineering, Autoignition temperature, Mechanics, Combustion, Fuel injection, law.invention, Ignition system, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, law, Combustor, symbols, Ignition timing
Abstract

著者人数: 6名, 資料番号: AC1000020000

Published
1997
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36. Mach 6 Testing of a Scramjet Engine Model

Author

Tetsuo Hiraiwa, Sadatake Tomioka, Tohru Mitani, Takeshi Kanda, and Nobuo Chinzei

Subjects
Engineering, business.industry, Mechanical Engineering, Aerospace Engineering, Thrust, Unstart, Combustion, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, Drag, symbols, Combustor, Scramjet, Aerospace engineering, business, Ramjet
Abstract

著者人数: 5名, 資料番号: AC1000019000

Published
1997
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38. Experimental Evaluation of Mass Capture Ratio of Scramjet Inlets

Author

Tetsuo Hiraiwa, Takeshi Kanda, Muneo Izumikawa, and Tohru Mitani

Subjects
geography, Materials science, geography.geographical_feature_category, Mechanical Engineering, Aerospace Engineering, Young's modulus, Mechanics, Propulsion, Inlet, Discharge coefficient, symbols.namesake, Fuel Technology, Space and Planetary Science, Swept wing, symbols, Scramjet
Abstract

著者人数: 4名, 資料番号: AC1000028000

Published
2004

39. Parametric Study of Airframe-Integrated Scramjet Cooling Requirement

Author

Goro Masuya, Takeshi Kanda, Akio Kanmuri, Yoshio Wakamatsu, and Nobuo Chinzei

Subjects
Propellant, Drag coefficient, Engineering, business.industry, Mechanical Engineering, Aerospace Engineering, Coolant, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, Airframe, symbols, Dynamic pressure, Scramjet, Aerospace engineering, business, Parametric statistics
Abstract

著者人数: 5名, 資料番号: AC1000012000

Published
1991

40. Experimental Study of a Combined-Cycle Engine Combustor in Ejector-Jet Mode

Author

Kanenori Kato, Atsuo Murakami, Kouichiro Tani, Kenji Kudo, and Takeshi Kanda

Subjects
Propellant, Materials science, business.product_category, Waste management, Mechanical Engineering, Aerospace Engineering, Pitot tube, Mechanics, Combustion, Fuel injection, law.invention, Fuel Technology, Rocket, Space and Planetary Science, law, Combustor, Supersonic speed, Duct (flow), business, Ramjet
Abstract

44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006, 資料番号: AC1000084000, レポート番号: AIAA-2006-0223

Published
2006
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41. Experimental Studies of Supersonic Film Cooling with Shock Wave Interaction (II)

Author

Fumiei Ono and Takeshi Kanda

Subjects
Fluid Flow and Transfer Processes, Shock wave, Materials science, Mechanical Engineering, Aerospace Engineering, Static pressure, Mechanics, Condensed Matter Physics, symbols.namesake, Flow separation, Mach number, Space and Planetary Science, symbols, Oblique shock, Supersonic speed, Ramjet, Choked flow
Abstract

資料番号: AC1000041000

Published
1997

42. Payload to Low Earth Orbit by Aerospace Plane with Scramjet Engine

Author

Takeshi Kanda and Kenji Kudo

Subjects
Physics, Geostationary transfer orbit, Payload, business.industry, Mechanical Engineering, Aerospace Engineering, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, symbols, Rocket engine, Aerospace engineering, Aerospace, business, Orbit insertion, Landing gear, Medium Earth orbit
Abstract

著者人数: 2名, 資料番号: AC1000018000

Published
1997
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43. Impulse function and drag in scramjet inlet models

Author

Tomoyuki Komuro, Atsuo Murakami, Nobuo Chinzei, Takeshi Kanda, Kouichiro Tani, and Kenji Kudo

Subjects
Propellant, Materials science, business.industry, Mechanical Engineering, Ram accelerator, Aerospace Engineering, Static pressure, Fuel Technology, Space and Planetary Science, Drag, Swept wing, Mass flow rate, Scramjet, Aerospace engineering, business, Wind tunnel
Abstract

著者人数: 6名, 資料番号: AC1000017000

Published
1996

44. Effect of Regenerative Cooling on Rocket Engine Specific Impulse

Author

Nobuo Chinzei, Takeshi Kanda, Goro Masuya, Yoshio Wakamatsu, Akio Kanmuri, and Masayuki Niino

Subjects
Engineering, business.industry, Liquid-propellant rocket, Mechanical Engineering, Rocket engine nozzle, Nozzle, Aerospace Engineering, Mechanics, Coolant, Fuel Technology, Space and Planetary Science, Specific impulse, Supersonic speed, Rocket engine, Combustion chamber, Aerospace engineering, business
Abstract

著者人数: 6名, 資料番号: AC1000015000

Published
1994

46. Propellant feed system of a regeneratively cooled scramjet

Author

Takeshi Kanda, Goro Masuya, and Yoshio Wakamatsu

Subjects
Propellant, Engineering, genetic structures, business.industry, musculoskeletal, neural, and ocular physiology, Mechanical Engineering, Aerospace Engineering, Thrust, Mechanics, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, Combustor, symbols, Scramjet, Specific impulse, Combustion chamber, Aerospace engineering, business, human activities, Ramjet
Abstract

著者人数: 3名, 資料番号: AC1000011000

Published
1991
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47. Mach 4 testing of scramjet inlet models

Author

Goro Masuya, Yoshio Wakamatsu, Kouichiro Tani, Tomoyuki Komuro, Takeshi Kanda, Kenji Kudo, Nobuo Chinzei, and Atsuo Murakami

Subjects
geography, Materials science, geography.geographical_feature_category, business.industry, Mechanical Engineering, Aerospace Engineering, Mechanics, Static pressure, Inlet, Flow separation, symbols.namesake, Fuel Technology, Mach number, Space and Planetary Science, Mass flow rate, Swept wing, symbols, Environmental science, Scramjet, Aerospace engineering, business, Wind tunnel
Abstract

ASME, SAE, and ASEE, Joint Propulsion Conference, 25th, Monterey, CA, July 10-13, 1989, 資料番号: AC1000089000, レポート番号: AIAA-1989-2680

Published
1989
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