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Start Over Author "Takeshi Kanda" Publisher american institute of aeronautics and astronautics
55 results on '"Takeshi Kanda"'

2. 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

3. 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

4. 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

5. 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

6. 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

7. 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

8. 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

9. 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

10. 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

11. 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

12. 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

13. 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

15. 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

17. Recent Progress in Scramjet/Combined Cycle Engines at JAXA Kakuda Space Center

Author

Shuichi Ueda, Kouichiro Tani, Katsuhiro Ito, Shigeru Sato, Tetsuo Hiraiwa, Sadatake Tomioka, and Takeshi Kanda

Subjects
Engineering, business.industry, Combined cycle, Aerospace Engineering, Thrust, Aerodynamics, Propulsion, Automotive engineering, law.invention, symbols.namesake, Mach number, law, symbols, Combustor, Environmental science, Rocket engine, Scramjet, Aerospace engineering, business
Abstract

This report presents recent research activities of the Combined Propulsion Research Group of Japan Aerospace Exploration Agency. Aerodynamics and combustion of the scramjet engine and the rocket–ramjet combined-cycle engine, structure and material for the two engines and thermo-aerodynamic of a re-entry vehicle are major subjects. In Mach 6 condition tests, a scramjet engine model produced about 2000 N net thrust, whereas a model produced thrust almost equal to its drag in Mach 12 condition. A flight test of a combustor model was conducted with Hyshot-IV. A rocket–ramjet combined-cycle engine model is under construction with validation of the rocket engine component. Studies of combustor models and aerodynamic component models were conducted for demonstration of the engine operation and improvement of its performances. Light-weight cooling panel by electrochemical etching examined and C / C composite structure was tested. Thermo-aerodynamics of re-entry vehicle was investigated and oxygen molecular density was measured also in high enthalpy flow.

Published
2006
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18. Aerodynamic Characteristics of the Modified Combined Cycle Engines in Ejector-Jet Mode

Author

Takeshi Kanda, Kouichiro Tani, and Shinichiro Tokudome

Subjects
Jet (fluid), Engineering, business.industry, Thrust, Pitot tube, Injector, Aerodynamics, Mechanics, Structural engineering, law.invention, law, Drag, Total pressure, business, Transonic
Abstract

44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006, 資料番号: AC1000085000, レポート番号: AIAA-2006-0224

Published
2006
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19. 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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20. 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

21. Design of Sub-scale Rocket-Ramjet Combined Cycle E

Author

Kouichiro Tani, Takeshi Kanda, Yoshio Wakamatsu, Shuichi Ueda, and Sadatake Tomioka

Subjects
business.product_category, Scale (ratio), Rocket, business.industry, Combined cycle, law, Environmental science, Aerospace engineering, business, Ramjet, law.invention
Published
2005
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23. Concept Study of High-reliable LH2/LOX Rocket Engi

Author

Moriyasu Fukuzoe, Masaaki Yasui, Hirotaka Kure, Makoto Yoshida, Hiroshi Aoki, Takeshi Kanda, Yoshihiro Naruo, and Keiichi Hasegawa

Subjects
Engineering, business.product_category, Rocket, business.industry, Aerospace engineering, business
Published
2005
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24. Multidisciplinary Design Optimization of SSTO Space Plane Considering Rigid Body Characteristics

Author

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

Subjects
Plane (geometry), Computer science, Multidisciplinary design optimization, Geometry, Space (mathematics), Rigid body
Abstract

43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 10-13, 2005, 資料番号: AC1000083000, レポート番号: AIAA-2005-0710

Published
2005
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25. Momentum Balance Model of Flow Field with Pseudo-Shock

Author

Takeshi Kanda and Kouichiro Tani

Subjects
Physics, Classical mechanics, Reaction, Astrophysics::High Energy Astrophysical Phenomena, Momentum balance, Outflow boundary condition, Outflow, Duct (flow), Inflow, Mechanics, Impulse function, Flow field, Astrophysics::Galaxy Astrophysics
Abstract

43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 10-13, 2005, 資料番号: AC1000080000, レポート番号: AIAA-2005-1045

Published
2005
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26. Aerodynamic Characteristics of the Combined Cycle Engine in an Ejector Jet Mode

Author

Takeshi Kanda, Kouichiro Tani, and Shin-ichiro Tokutome

Subjects
Engineering, Jet (fluid), business.industry, Mass flow, Nozzle, Mechanical engineering, Pitot tube, Injector, Aerodynamics, Mechanics, law.invention, law, Drag, business, Transonic
Abstract

43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 10-13, 2005, 資料番号: AC1000082000, レポート番号: AIAA-2005-1210

Published
2005

27. Experimental Study of Downstream Combustion Ramjet-Mode

Author

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

Subjects
Materials science, Downstream (manufacturing), Mode (statistics), Mechanics, Combustion, Ramjet
Abstract

43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 10-13, 2005, 資料番号: AC1000081000, レポート番号: AIAA-2005-0617

Published
2005

28. 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

29. Scramjet Mode Tests of a Combined Cycle Engine Combustor

Author

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

Subjects
Propellant, Materials science, Engine configuration, business.industry, Rocket engine nozzle, Combustor, Rocket engine, Scramjet, Aerospace engineering, Fuel injection, business, Ramjet
Abstract

12th AIAA International Space Planes and Hypersonic Systems and Technologies, Norfolk, Virginia, Dec. 15-19, 2003, 資料番号: AC1000065000, レポート番号: AIAA-2003-7051

Published
2003
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30. Scramjet Performance Achieved in Engine Tests from M4 to M8 Flight Conditions

Author

Takeshi Kanda, Nobuo Chinzei, Tohru Mitani, Sadatake Tomioka, and Toshinori Kouchi

Subjects
Hypersonic speed, Engineering, Mach number, air capture ratio, business.industry, 空気捕捉比, マッハ数, boundary layer, 境界層, 推力, 性能試験, scramjet engine, スクラムジェットエンジン, Aeronautics, performance test, 化学量論比, thrust, Scramjet, Aerospace engineering, stoichiometric ratio, business
Abstract

Thrust performances of scramjet engines were compared with theoretical values to quantify the progress in engine performances (defined as achievement factors, or factors) from Mach (termed as M) 4 to M8 flight conditions. An engine with a ramp produced a net thrust of 215 N under the M8 tests and a comparison of a theoretical thrust yielded a thrust achievement factor of 51 percent. By excluding boundary layer, an engine with a thick strut delivered a net thrust of 560 N and showed a thrust factor of 92 percent and a net thrust factor of 45 percent. The thrusts were limited by flow separation caused by engine combustion (termed as engine unstart). The starting characteristics were improved by boundary layer controls in M6 and M4 conditions. An engine with a thin strut doubled the thrust from 1,620 N to 2,460 N by the boundary layer bleeding in the M6 tests. The improved thrust factor was 60 percent at the stoichiometric H2 condition. Under M4 tests, the net thrust was tripled by the bleed and a two-staged injection of H2. As results, the thrust factor was raised from 53 percent to 70 percent, the net thrust factor was increased from 32 percent to 55 percent. Studies required for improving the net performance were addressed., ISSNの誤記: 1349-1148, Incorrect ISSN: 1349-1148, 資料番号: AA0047412000, レポート番号: JAXA-RR-03-020E

Published
2003
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32. Effect of Ingested Boundary Layer on Scramjet Engines' Thrust and Combustion Characteristics

Author

Masatoshi Kodera, Takeshi Kanda, Kanenori Kato, Toshihito Saito, Kan Kobayashi, and Tetsuo Hiraiwa

Subjects
Engineering, business.industry, Thrust, Boundary layer suction, Combustion, Boundary layer, Flow separation, symbols.namesake, Mach number, Inviscid flow, symbols, Scramjet, Aerospace engineering, business
Abstract

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, July 20-23, 2003, 資料番号: AC1000095000, レポート番号: AIAA-2003-4739

Published
2003
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33. Experimental Investigation of an Ejector-Jet

Author

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

Subjects
Jet (fluid), law, Environmental science, Mechanics, Injector, law.invention
Abstract

41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 6-9, 2003, 資料番号: AC1000078000, レポート番号: AIAA-2003-0188

Published
2003

34. Measurement of mass capture ratio of scramjet inlet models

Author

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

Subjects
Thesaurus (information retrieval), geography, geography.geographical_feature_category, business.industry, Computer science, Scramjet, Aerospace engineering, business, Inlet
Abstract

41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 6-9, 2003, 資料番号: AC1000079000, レポート番号: AIAA-2003-0011

Published
2003

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

Author

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

Subjects
Leading edge, Engineering, business.industry, Airflow, Pitot tube, Mechanics, law.invention, Physics::Fluid Dynamics, Boundary layer, symbols.namesake, Mach number, Drag, law, symbols, Hypersonic wind tunnel, Aerospace engineering, business, Wind tunnel
Abstract

21st AIAA Applied Aerodynamics Conference, Orlando, Florida, June 23-26, 2003, 資料番号: AC1000086000, レポート番号: AIAA2003-3420

Published
2003

36. 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

37. Experiments on a Scramjet Engine with Ramp-Compression Inlet at Mach 8 Condition

Author

Yoshinari Enomoto, Tetsuo Hiraiwa, Takeshi Kanda, and Tohru Mitani

Subjects
Engineering, business.industry, Mechanical engineering, Thrust, Compression (physics), symbols.namesake, Mach number, Heat flux, Drag, Combustor, symbols, Scramjet, Aerospace engineering, business, Ramjet
Abstract

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, Indiana, July 7-10, 2002, 資料番号: AC1000097000, レポート番号: AIAA-2002-4129

Published
2002
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38. A Conceptual Study of a Combined Cycle Engine for an Aerosapce Plane

Author

Takeshi Kanda and Kenji Kudo

Subjects
Engineering, Combined cycle, law, business.industry, Plane (geometry), Aerospace engineering, Aerospace, business, Conceptual study, law.invention
Abstract

AIAA/AAAF 11th International Space Planes and Hypersonic Systems and Technologies Conference, Orleans, France, Sep. 29-4, 2002, 資料番号: AC1000064000, レポート番号: AIAA-2002-5146

Published
2002

39. Modified water-cooled scramjet engine tested under M8 Condition

Author

Takeshi Kanda, Kan Kobayashi, Toshihito Saito, Sadatake Tomioka, Tetsuo Hiraiwa, and Kouichiro Tani

Subjects
Engineering, Thesaurus (information retrieval), Search engine, business.industry, Water cooled, Scramjet engine, business, Automotive engineering
Abstract

AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 37th, Salt Lake City, UT, July 8-11, 2001, 資料番号: AC1000098000, レポート番号: AIAA-2001-3202

Published
2001
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40. Dual-Mode Operation in a Scramjet Combustor

Author

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

Subjects
Materials science, business.industry, Mechanics, Combustion, Fuel injection, symbols.namesake, Mach number, Total air temperature, Combustor, symbols, Duct (flow), Scramjet, Aerospace engineering, Total pressure, business
Abstract

AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference, 10th, Kyoto, Japan, Apr. 24-27, 2001, 資料番号: AC1000063000, レポート番号: AIAA-2001-1816

Published
2001

41. Effect of airframe geometry on thrust performance of aerospace plane

Author

Masatoshi Kodera, Kouichiro Tani, and Takeshi Kanda

Subjects
Plane (geometry), business.industry, Airframe, Thrust, Aerospace engineering, Aerospace, business, Geology
Abstract

AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 36th, Huntsville, AL, July 16-19, 2000, 資料番号: AC1000099000, レポート番号: AIAA-2000-3342

Published
2000
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42. Mach 8 testing of a scramjet engine with ramp compression

Author

Takeshi Kanda, Noboru Sakuranaka, Fumiei Ono, Atsuo Murakami, Muneo Izumikawa, and Yoshio Wakamatsu

Subjects
symbols.namesake, Materials science, Mach number, business.industry, symbols, Aerospace engineering, business, Compression (physics), Scramjet engine
Abstract

Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan. 10-13, 2000, 資料番号: AC1000076000, レポート番号: AIAA-2000-0616

Published
2000
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44. Effect of Airframe Integrated Configuration on Scramjet Inlet Performance

Author

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

Subjects
Materials science, Drag, business.industry, Airframe, Dynamic pressure, Scramjet, Thrust, Aerodynamics, Mechanics, Total pressure, Aerospace engineering, business, Wind tunnel
Abstract

Aerospace Sciences Meeting and Exhibit, 38th, Reno, NV, Jan. 10-13, 2000, 資料番号: AC1000075000, レポート番号: AIAA-2000-0619

Published
2000

45. Mach 8 testing of scramjet engine models

Author

Muneo Izumikawa, Takeshi Kanda, Atsuo Murakami, Yoshio Wakamatsu, Kenji Kudo, and Fumiei Ono

Subjects
symbols.namesake, Materials science, Mach number, business.industry, symbols, Scramjet, Aerospace engineering, business, Scramjet engine
Abstract

Aerospace Sciences Meeting and Exhibit, 37th, Reno, NV, Jan. 11-14, 1999, 資料番号: AC1000074000, レポート番号: AIAA-1999-0617

Published
1999
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46. Effects of Propellant Characteristics and Vehicle Structure on Rocket Space Plane

Author

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

Subjects
Propellant, Physics, Propellant tank, business.product_category, Rocket, business.industry, Specific impulse, Rocket propellant, Propulsion, Aerospace engineering, Mass ratio, business, Ramjet
Abstract

AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 9th, Norfolk, VA, Nov. 1-5, 1999, 資料番号: AC1000061000, レポート番号: AIAA-1999-4867

Published
1999

47. Scramjet Inlet Flow Computations by Hybrid Grid Method

Author

Masatoshi Kodera, Kazuhiro Nakahashi, Tohru Mitani, Tetsuo Hiraiwa, and Takeshi Kanda

Subjects
Physics, Finite volume method, Turbulence, business.industry, Airflow, Inflow, Unstart, Physics::Fluid Dynamics, symbols.namesake, Mach number, symbols, Combustor, Scramjet, Aerospace engineering, business
Abstract

Aerospace Sciences Meeting and Exhibit, 36th, Reno, NV, Jan. 12-15, 1998, 資料番号: AC1000073000, レポート番号: AIAA-1998-0962

Published
1998

48. Geometrical effects to aerodynamic performance of scramjet engine

Author

Kouichiro Tani, Takeshi Kanda, Tetsuji Sunami, Tetsuo Hiraiwa, and Sadatake Tomioka

Subjects
Overall pressure ratio, Drag coefficient, Materials science, business.industry, Aerodynamics, Mechanics, Combustion, Compression (physics), symbols.namesake, Mach number, Compression ratio, symbols, Scramjet, Aerospace engineering, business
Abstract

AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 33rd, Seattle, WA, July 6-9, 1997, 資料番号: AC1000104000, レポート番号: AIAA-1997-3018

Published
1997
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49. Testing of a scramjet engine model in Mach 6 vitiated air flow

Author

Tetsuo Hiraiwa, Shigeru Sato, Sadatake Tomioka, Takeshi Kanda, Takashi Shimura, and Tohru Mitani

Subjects
symbols.namesake, Mach number, business.industry, Airflow, symbols, Environmental science, Aerospace engineering, Scramjet engine, business
Abstract

Aerospace Sciences Meeting and Exhibit, 35th, Reno, NV, Jan. 6-9, 1997, 資料番号: AC1000072000, レポート番号: AIAA-1997-0292

Published
1997
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50. Scramjet engine testing in Mach 6 vitiated air

Author

Tohru Mitani, Takeshi Kanda, Kouichiro Tani, Toshihito Saito, Tetsuji Sunami, Shigeru Sato, Sadatake Tomioka, and Tetsuo Hiraiwa

Subjects
symbols.namesake, Mach number, business.industry, symbols, Environmental science, Scramjet, Aerospace engineering, Scramjet engine, business
Published
1996
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