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1990 Fiscal Year Final Research Report Summary

Studies of AOTV's Gasdynamics

Research Project

Project/Area Number 63302022
Research Category

Grant-in-Aid for Co-operative Research (A)

Allocation TypeSingle-year Grants
Research Field Aerospace engineering
Research InstitutionKyushu University (1989-1990)
Kyoto University (1988)

Principal Investigator

NIDHIDA Michio  Kyushu Univ. Faculty of Eng., Professor, 工学部, 教授 (10025968)

Co-Investigator(Kenkyū-buntansha) ASO Shigeru  Kyushu Univ., Faculty of Eng., Associate Prof., 工学部, 助教授 (40150495)
TESHIMA Koji  Kyoto Univ. of Education, Faculty of Education, Prof, 教育学部, 教授 (90026104)
HONMA Hiroki  Chiba Univ., Faculty of Eng., Professor, 工学部, 教授 (90009233)
SHIRAI Hiroyuki  Gunma Univ., Faculty of Eng., Professor, 工学部, 教授 (00008509)
FUJIWARA Toshitaka  Nagoya Univ., Faculty of Eng., Professor, 工学部, 教授 (90023225)
Project Period (FY) 1988 – 1990
KeywordsSpace / Space Vehicle / Opposing jet / Real Gas Effect / Rarefied Gas Dynamics / Thermal Protection
Research Abstract

"AOTV" means Aeroassisted Orbital Transfer Vehicle. A space vehicle decelerates by aerobraking when it transfers from a higher orbit to a lower orbit. This study was conducted by 20 investigators. The AOTV includes the following problems : (1) shock layer interaction, (2) real gas effect, (3) rarefied gas effect and (4) thermal protection.
The results of this study are summarized as follows :
(1) Shock layer interaction : Flow field of an interaction of an opposing jet and a supersonic free stream was observed by LIF flow visualization technique. It was observed that when the jet to free stream stagnation pressure ratio is small, a free stream shock, contact surface and Mach disk periodically moves in the flow direction. This oscillation was confirmed in the numerical simulation.
(2) Real gas effect : Effect of dissociation, ionization and radiation was investigated for the flows at a Mach number larger than 20. It is seen that the real gas effect decreases the shock distance of a blunt body and also that the temperature profile in the shock layer is significantly influenced by the real gas effect.
(3) Rarefied gas effect : numerical simulation of low density flows over a blunt body was made by direct Monte Carlo simulation and by numerically solving Boltzmann equation. For the purpose of investigating the flight in a low density atmosphere, the performance test of a ballistic range facility was conducted.
(4) Thermal protection : the surface heat transfer and the effect of the wall catalyst was investigated experimentally and numerically. In particular, it is seen that non-catalytic wall decreases surface heat transfer.

  • Research Products

    (57 results)

All Other

All Publications (57 results)

  • [Publications] M. Nishida & S. Ishimaru: "Numerical Analysis of Gas-Solid Two-Phase Nonequilibrium Nozzle Flows" JSME International J.Vol. 33. 494-500 (1990)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] M. Nishida, K. Teshima, K. Ueno & S. Tanaka: "Shock Waves Generated by an Opposing Jet" Current Topics in Shock Waves. 114-119 (1990)

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      「研究成果報告書概要(欧文)」より
  • [Publications] M. Nishida & Y. Sakamura: "Hypersonic Flows with Air Chemistry over a Reentry Vehicle at High Altitudes" Proc. 17th Int. Symp. on Space Technolog and Science. 729-734 (1990)

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  • [Publications] Y. Sakamura & M. Nishida: "Numerical Calculation of Thermal and Chemical Nonequilibrium flows around a Hypersonic Reentry Vehicle" Trans. Jpn Soc. Aero. and Space Sci.

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      「研究成果報告書概要(欧文)」より
  • [Publications] K. Teshima: "Three Dimensional Structure of a Supersonic ^<11>Free Jet Issuing from a Rectangular Orifice" Numerical Method in Fluid Dynamics. II. 993-999 (1990)

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  • [Publications] K. Kuzuzu & H. Kubota: "Effects of Gas-Surface Interaction Models on Aerodynamic Characteristics" Jrans Jpn Soc Aero. and Space Sci.

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  • [Publications] K. Teshima: "Radically Directed Underexpanded Jet from a Ring-Shaped Nozzle" Rarefied Gas Dynamics, Progress in Astronautics and Aeronautics. Vol. 116. 378-390 (1989)

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  • [Publications] N. Arai & T. Tani: "Active control of vortex shedding frequency by a splitter plate" Proc. Int. Cong. Recent Development in Air and Structure Borne Sound and Vibration.

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  • [Publications] H. Tahara, Y. Kagaya & T. Yoshikawa: "Quasisteady Magnetoplasma-dynamic Thruster with Applies Magnetic Fields for Near-Earth Missions" J. Propulsion and Power. Vol. 5. 713-717 (1989)

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  • [Publications] Y. Tsubakishita, T. Kitagawa & T. Yoshikawa: "Fast-Adaptive Grid Method for Compressible Flows" Trans. JSASS. Vol. 30. 217-227 (1990)

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  • [Publications] H. Tokunaga, K. Ichinose & N. Satofuka: "Numerical Simulation of Transition to Turbulence Using Higher Order Method of Line" Proc. 12th Int. Conf. Numerical Methods in Fluid Dynamics.

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  • [Publications] H. Tokunaga, K. Ichinose & N. Satofuka: "N Satofuka, Numerical Simulation of Instability of Plane Flow Using Eighth Order Accurate Method of Line" Mem. Fac. Eng. Design, Kyoto Inst. Tech.Vol. 39. 19-30 (1991)

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  • [Publications] M. Shinada, H. Tokumaga, N. Satofuka & N. Nishida.: "Numerical Simulation of Three-Dimensional Viscous Flows Using the Vector Potential Method" JSME International J.Vol. 34-B.

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  • [Publications] H. Tokunaga, K. Ichinose & N. Satofuka: "Direct Simulation of Transient Turbulence Flows Using Generalized Method of Line" Proc. let ASME-JSME Fluid Eng. Conf.

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  • [Publications] H. Tokunaga, K. Yoeda & N. Satofuka: "Direct Simulation of Three-Dimensional Flows Using Generalized Vector Potential Method" Proc. AIAA 10th Comp. Fluid Dynamics Conf.

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  • [Publications] M. Takahashi & A. Hayashi: "Numerical Study on the Chemically Reacting Jet in a Supersonic Flow" Proc. 2nd Japan-USSR Joint Symp. Comp. Fluid Dynamics.

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  • [Publications] A. Hayashi & M. Takahashi: "Numerical Study on Mixture and Combusting of Injection Hydrogen Jet in a Supersonic Air Flow" J. Propulsion and Power.

    • Description
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  • [Publications] A. Hayashi & M. Takahashi: "Three-Dimensional Calculation of a Hydrogen Jet Injection into a Supersonic Air Flow" Progress in Astro. and Aero.

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  • [Publications] Y. Inoiue, A. Hayashi, T. Fujiwara, T. Miyake: "T. Katsurahara, Numerical Analysis of RCS Jets in Hypersonic Flights" Proc. Int. Pacific Air & Space Tech. Conf. 1991.

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  • [Publications] N. Tsuboi, A. Hayashi, T. Fujiwara, K. Arashi & M. Kodama: "Numerical Simulation of a Supersonic Jet Impingement on a Ground" Proc. Int. Pacific Air & Space Tech. 1991.

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  • [Publications] Y. Takano & O. Ashida: "Numerical Simulation on Failure Processes of Detonation Waves Propagating in an Expanding channel" JSME International J.Vol. 33. 114-121 (1990)

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  • [Publications] Y. Takano: "Simulations for Ionizing Reflected-Shock Waves in Argon in a Shock Tube" AIP Conf. Proc.Vol. 208. 408-413 (1990)

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  • [Publications] Y. Takano: "Simulations of Bifurcation Process of Reflected Shock Waves in Ionizing Argon in a Shock Tube" Computers and Fluids.

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  • [Publications] K. Yamamoto & T. Sanryo: "Flow of a Rarefied Gas Past a Two-Dimensional Body of an Arbitrary Shape at Small Mch Number" Rarefied Gas Dynamics.

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  • [Publications] H. Iizuka, H. Honma, A. Tsukamoto & T. Ohno: "Two-Dimensional Feature of Strong Shock Waves in Gases" Proc. 17th Int. Symp. Shock Waves and Shock Tubes. 856-861 (1990)

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  • [Publications] H. Honma, A. Tsukamoto & D. O. Xu: "Continuum and Kinetic-Model Approaches in Numerical Simulation of Shock Waves Moving along a Plane Wall" Proc. USSR-Japan Symp. Comp. Fluid Dynamics, 1988. 148-154 (1989)

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  • [Publications] H. Honma, A. Tsukamoto, T. Ohno & Tanaka: "Generation and Observation of Strong Shock Waves in the Flight Regimes of AOTV" ISAS Report. SP-7. 3-14 (1988)

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  • [Publications] T. Abe: "A Self-consistent Tension Shell Structure for Application to Aerobraking Vehicle and Its Aerodynamic Characteristics" AIAA-88-3403.(1988)

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  • [Publications] T. Abe: "Rarefied Gas Flows Analysis by Direct Simulation Monte Carlo Method in Body-Fitted Coordinate System" J. Comp. Phys.424-432 (1989)

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  • [Publications] T. Shimada & T. Abe: "Applicability of the Direct Simulation Monte Carlo Method in Body Fitted Coordinate System" Progress in Astro. Aero.Vol. 118. 258-270 (1989)

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  • [Publications] T. Abe, J. Kawaguchi, K. Uesugi and C. W. Yen: "Aerobraking Stragies for the Sample of Comet Coma Earth" Proc. 17th Int. Symp. on Space Tech. and Sci. 653-660 (1990)

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  • [Publications] T. Abe: "Modification of Nanbu's Method of DSMC by Using the Null-collision Technique" Proc. Int. Symp. on Rarefied Gas Dynamics.

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  • [Publications] T. Abe: "Anomalous Collision Rate in Direct Simulation Monte Carlo Method" Phys. Fluids.

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  • [Publications] Y. Yoshizawa & U. Inoue: "Potential Flow Calculation of Lift and Moment to a Flapping Wing" Proc. SU-Japan Joint Cymp. on Comp. Fluid Dynamics. Vol. 1. 95-101 (1989)

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  • [Publications] Y. Yoshizawa & Y. Hozumu: "Numerical Calculation of Viscous Flows in and around a Liquid Droplet" Numerical Methods in Fluid Dynamics. 238-243 (1989)

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  • [Publications] Y. Hozumu and Y. Yoshhizawa: "Numerical Analysis of Dust Particles Motion inside Gas Bubble for Flue Gas Desulfurization in Jet Bubbling Reactor" Computers and Fluids.

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  • [Publications] K. Sunada, A. Yabe, T. Taketani & Y. Yoshhizawa: "Experimental Study of EHD Pseudo-Dropwise Condensation" 3rd ASME-JSME Thermal Eng. Joint Conf.

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  • [Publications] Y. Hozumu & Y. Yoshizawa: "Numerical Analysis of Dust Particles Collision in Bubbling and Spray Methods" lst ASME-JSME Fluid Eng. Joint Conf,.

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  • [Publications] M. Watanabe & K. Takayama: "Converging Cylindrical Shock Wave" Phys. Fluids A.Vol. 2. 1521 (1990)

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  • [Publications] T. Matsumura, O. Onodera & K. Takayama: "Recent Research Activities at SWRC : Optical Flow Visualization of Flying Projectiles" Proc. 41st Aeroballistic Range Association Meeting.

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  • [Publications] M. Hayashi, S. Aso & A. Tan: "Aerodynamic Heating in the Interaction Regions of Shock Waves and Turbulent Boundary Layers Induced by Sharp Fins" Mem. Fac. Eng. Kyushu Univ.Vol. 49. 69-80 (1989)

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      「研究成果報告書概要(欧文)」より
  • [Publications] M. Hayashi & S, Aso & T. Tan: "Fluctuation of Heat Transfer in Shock Wave/Turbulent Boundary Layer Interaction" AIAA J.Vol. 27. 399-404 (1989)

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  • [Publications] S. Aso & A. Tan & M. Hayashi: "The Structure of Aerodynamic Heating in Three-Dimensional Shock Wave/Turbulent Boundary Layer Interaction Induced by Sharp and Blunt Fins" AIAA-89-1854. (1989)

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  • [Publications] S. Aso, A. Tan & M. Hayashi: "Aerodynamic Heating in Shock Wave/Boundary Layer Interaction Regions Induced by Blunt Fins" Mem. Fac. Eng. Kyushu Univ.Vol. 49. 109-124 (1989)

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  • [Publications] S. Aso, S. Kuranaga, S. Nakao, A. Tan & M. Hayashi: "A Study of Aerodynamic Heating in Sweptback Blunt Fin Induced Shock Wave/Turbulent Boundary Layer Interactions" Proc. Int. Session Japan Soc. Aero. Space Sci. 27th Aircraft Symp.590-593 (1989)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] S. Aso, S. Kuranaga, S. Nakao & M. Hayashi: "Aerodynamic Heating Phenomena in Three-Dimensional Shock Wave/Turbulent Boundary Layer Interaction Induced by Sweptback Fins" AIAA 90-0381. (1989)

    • Description
      「研究成果報告書概要(欧文)」より
  • [Publications] S. Aso. S. Aso & S. Kuranaga: "Aerodynamic Heating in the Interaction Regions of Shock Waves and Turbulent Boundary Layers Induced by Swept Blunt Fins" Mem. Fac. Eng. Kyushu Univ. Vol. 50. 121-134 (1990)

    • Description
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  • [Publications] S. Aso, Y. Tanahashi, A. Tan & M. Hayashi: "Experimental and Computational Studies on Unsteady Aerodynamic Heating Phenomena in Shock Reflection Process" Mem. Fac. Eng. Kyushu Univ.Vol. 50. 295-308 (1990)

    • Description
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  • [Publications] S. Aso, S. Nakao, S. Kuranaga & M. Hayashi: "A Fundamental Study on Aerodynamic Heating in Conjunction of Fin-Body and Wing-Body Conjunctions" Proc. China-Japan Joint Symp. on Aerodynamics and Aircraft Design. 50-54 (1990)

    • Description
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  • [Publications] S. Aso, M. Hayashi & A. Tan: "Experimental and Computational Studies on Unsteady Aerodynamic Heating Induced by Shock Reflections" Proc. China-Japan Joint Symp. on Aerodynamics and Aircraft Design. 126-130 (1990)

    • Description
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  • [Publications] S. Aso, M. Hayashi, A. Tan & Y. Tanahashi: "Surface Heat Transfer Change Induced by Unsteady Shock Reflections and Numerical Simulation on Shock Reflections" Proc. 17th Int. Symp. Shock Waves and Shock Tubes. 630-635 (1990)

    • Description
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  • [Publications] S. Aso, S. Nakao, S. Kuranaga & M. Hayashi: "Experimental Investigation on Turbulent Phenomena in Three-Dimensional Shock Wave/Turbulent Boundary Layer Interaction Induced by Blunt Fin" Proc. 17th Int. Symp. Space Tech. and Sci.777-782 (1990)

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  • [Publications] S. Aso and M. Takano: "Numerical Simulation of Shock Reflections by a TVD Scheme" Proc. 17th Int. Symp. Space Tech. and Sci.783-788 (1990)

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  • [Publications] S. Aso, A. Tan, M. Takano & M. Hayashi: "Numerical Simulations of Unsteady Shock Reflections by Ramps" Proc. ISCFD, Nagoya. 518-522 (1990)

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  • [Publications] H. Tokunaga, N. Satofuka & H. Tanida: "Higher Order Accurate Computations of the Sivashinsky Equation" Mem Fac. Eng. and Design Kyoto Inst. Tech.Vol. 37. 72-84 (1988)

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  • [Publications] H. Tokunaga, N. Satofuka & T. Yoshikawa: "Efficient Numerical Simulation of Viscous Flows along Airfoil using an Integro-Differential Method" Mem Fac. Eng. and Design Kyoto Inst. Thch.Vol. 38. 35-46 (1990)

    • Description
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  • [Publications] H. Tokunaga, K. Ichinose & N. Satofuka: "Numerical Simulation of Transient Turbulent Flows by Vorticity-Vector Potential Formulation" Computers and Fluids.

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Published: 1993-08-12  

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