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Your search keyword '"Takeshi Kanda"' showing total 15 results
Start Over Author "Takeshi Kanda" Publisher american institute of aeronautics and astronautics (aiaa)
15 results on '"Takeshi Kanda"'

1. 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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2. 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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3. 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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4. 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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5. 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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6. 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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7. 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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8. 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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9. 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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10. 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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12. Experimental studies of supersonic film cooling with shock wave interaction

Author

Yoshio Wakamatsu, Fumiei Ono, Masahiro Takahashi, Takeshi Kanda, and Toshihito Saito

Subjects
Shock wave, Adiabatic wall, Materials science, Aerospace Engineering, Thermodynamics, Heat transfer coefficient, Mechanics, Mach wave, Moving shock, symbols.namesake, Mach number, symbols, Oblique shock, Supersonic speed, Astrophysics::Galaxy Astrophysics
Abstract

ASME, SAE, and ASEE, Joint Propulsion Conference and Exhibit, 31st, San Diego, CA, July 10-12, 1995, 資料番号: AC1000101000, レポート番号: AIAA-1995-3141

Published
1996
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13. 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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14. 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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15. Evaluation of Effectiveness of Periodic Flight by a Hypersonic Vehicle

Author

Tetsuo Hiraiwa and Takeshi Kanda

Subjects
Physics, Hypersonic speed, Sounding rocket, Angle of attack, business.industry, Range (aeronautics), Trajectory, Aerospace Engineering, Dynamic pressure, Aerospace engineering, Kinetic energy, business, Potential energy
Abstract

P ERIODIC flight has been proposed for long-range optimal hypersonic cruises, and its effectiveness has been examined [1– 4].Most studies have investigated optimal periodic flight trajectories in a cyclic flight. Rudd [4] and others adopted damped-periodic flight trajectories with the constraint that the ratio of kinetic to potential energy remained the same at the endpoints of a period. Large potential energy due to a high altitude can increase the speed and the range of the vehicle, even when the vehicle speed is low. In the present study, the total of the kinetic and the potential energies was specified at the endpoint of the flight. With this constraint, ranges of the damped-periodic and the steady-state flights were compared. This constraint will be practically effective as the standard for the periodic flight of hypersonic vehicles.

Published
2007
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