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S. Aso · SciRah

Researcher profile · Semantic Scholar

S. Aso

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S. Aso — researcher profile on SciRah

h-index: 14
Works: 211
Citations: 1,107

Most-cited papers

Experimental Study on Thermal Protection System by Opposing Jet in Supersonic Flow
Kentaro Hayashi, S. Aso, Y. Tani
2006155 citations
Semantic Scholar
Numerical study of thermal protection system by opposing jet
K. Hayashi, S. Aso, Y. Tani
2005113 citations
Semantic Scholar
A study on supersonic mixing by circular nozzle with various injection angles for air breathing engine
S. Aso, Keinosuke Inoue, K. Yamaguchi, Y. Tani
200659 citations
Semantic Scholar
Fundamental study of supersonic combustion in pure air flow with use of shock tunnel
S. Aso, A. N. Hakim, S. Miyamoto, Keinosuke Inoue +1 more
200446 citations
Semantic Scholar
Reducing Aerodynamic Heating by the Opposing Jet in Supersonic and Hypersonic Flows
Isao Tamada, S. Aso, Y. Tani
201033 citations
Semantic Scholar
Numerical study on aerodynamic heating reduction by opposing jet
Kentaro Hayashi, S. Aso, Y. Tani
200622 citations
Semantic Scholar
Numerical study of the effect of the opposing jet on reduction of aerodynamic heating with different nose configurations
Isao Tamada, S. Aso, Y. Tani
200818 citations
Semantic Scholar
Reduction of aerodynamic heating with opposing jet through extended nozzle in high enthalpy flow
Naoki Morimoto, Jangsu Yoon, S. Aso, Y. Tani
201415 citations
Semantic Scholar
Effects of multi-section swirl injection method on fuel regression rate of high density polyethylene fueled hybrid rocket engine
Sho Ohyama, Y. Hirata, K. Araki, K. Ohe +3 more
201313 citations
Semantic Scholar
Hybrid Rocket Firing Experiments at Various Axial–Tangential Oxidizer-Flow-Rate Ratios
K. Ozawa, K. Kitagawa, S. Aso, T. Shimada
2019Journal of Propulsion and Power12 citations Open access
Semantic Scholar
Improvement of regression rate and combustion efficiency of high density polyethylene fuel and paraffin fuel of hybrid rockets with multi-section swirl injection method
Y. Hirata, S. Aso, T. Hayashida, Ryuji Nakawatase +3 more
201111 citations
Semantic Scholar
Reduction of aerodynamic interference for separation of two-stage reusable launch vehicles
Taro Uematsu, Takuro Ishida, S. Aso, Y. Tani
200911 citations
Semantic Scholar
Study of Cryogenic Mechanical Strength and Fracture Behavior of Adhesives for CFRP Tanks of Reusable Launch Vehicles
T. Shimoda, Jian-Mei He, S. Aso
200610 citations
Semantic Scholar
Experimental Study on Effects of Fuselage Configurations for RLV on Aerodynamic Characteristics
Wataru Morita, T. Yoneda, S. Aso, Y. Tani +1 more
200410 citations
Semantic Scholar
The effect of diaphragm opening time on the feasibility of tuned operation in free piston shock tunnels
M. Mizoguchi, S. Aso
20099 citations
Semantic Scholar
Hybrid Propulsion Technology Development in Japan for Economic Space Launch
T. Shimada, S. Yuasa, Harunori Nagata, S. Aso +14 more
20178 citations
Semantic Scholar
Reduction of aerodynamic heating and drag with opposing jet through extended nozzle in high enthalpy flow
Naoki Morimoto, S. Aso, Y. Tani
20148 citations
Semantic Scholar
Static burning tests on a bread board model of altering-intenisty swirling-oxidizer-flow-type hybrid rocket engine
K. Ozawa, T. Usuki, Genki Mishima, K. Kitagawa +8 more
20167 citations
Semantic Scholar
Visualization of flames in combustion chamber of hybrid rocket engine with multi-section swirl injection method
H. Tada, S. Aso, Y. Tani, Sho Ohyama +4 more
20147 citations
Semantic Scholar
A study on performance improvement of paraffin fueled hybrid rocket engines with multi-section swirl injection method
K. Araki, Y. Hirata, Sho Ohyama, K. Ohe +3 more
20137 citations
Semantic Scholar
A Study of Hybrid Rockets with Multi-Section Swirl Injection Method
Sho Ohyama, S. Aso, Y. Hirata, K. Araki +3 more
20127 citations
Semantic Scholar
Aerodynamic Interference Reduction Method for Two-Stage Launch Vehicles Supersonic Separation
Taro Uematsu, S. Aso, Y. Tani
20117 citations
Semantic Scholar
Active Control of Aerodynamic Characteristics of Space Transportation System by Lateral Blowing
K. Tadakuma, S. Aso, Y. Tani
20047 citations
Semantic Scholar
A Study on Reduction of Aerodynamic Heating by Opposing Jet in Supersonic Flow
Kentaro Hayashi, S. Aso
20047 citations Open access
Semantic Scholar
A STUDY ON NEW RAMP INJECTORS WITH SLOTTED NOZZLE FOR IMPROVEMENT OF SUPERSONIC MIXING
Keinosuke Inoue, S. Aso
20047 citations
Semantic Scholar
An experimental study on gust load alleviation using passive ventilation wing concept
Y. Tani, Shuhei Seki, S. Aso
20186 citations
Semantic Scholar
Supersonic Flight Separation Simulation For TSTO Launch Vehicles Considering Shock Wave Interaction Reduction
Taro Uematsu, S. Aso, Y. Tani
20126 citations
Semantic Scholar
A study on aerodynamic characteristics of lifting body and wing body configurations for fully reusable launch vehicles
S. Aso, Y. Tani, S. Tsuchiya, T. Yoneda +2 more
20046 citations
Semantic Scholar
Study on hybrid rocket with multi-section swirl injection method toward flight experiments of subscale space plane
K. Ohe, Masato Mizuchi, S. Aso, Y. Tani +4 more
20145 citations
Semantic Scholar
A Study on High Performance Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Space Propulsion System
S. Aso, Y. Tani, Tani Shohei Saiga, Ryohei Arakawa +1 more
20184 citations
Semantic Scholar
Experimental study of the morphing flap as a low noise high lift device for aircraft wing
Y. Tani, Y. Matsuda, A. Doi, Y. Yamashita +2 more
20124 citations
Semantic Scholar
A Study of Hybrid Rocket Engine with Multi-Section Swirl Injection Method
Sho Ohyama, S. Aso, Y. Hirata, K. Araki +3 more
20124 citations
Semantic Scholar
An Experimental Study on Base Pressure Correction for Bluff-Base Bodies Using Magnetic Suspension and Balance System
K. Tadakuma, S. Aso, Y. Tani, Yasushi Mizoguchi +1 more
20054 citations Open access
Semantic Scholar
A Study on Increase of Duration of a Free Piston Shock Tunnel
M. Mizoguchi, S. Aso, S. Futae, Kentaro Hayashi
20044 citations
Semantic Scholar
An Experimental Study on Passive Ventilation Wing with Porous Surfaces for Gust Load Alleviation
Shuhei Seki, Y. Tani, S. Aso
2019AIAA Scitech 2019 Forum3 citations
Semantic Scholar
Effect of Fuselage Cross Section on Aerodynamic Characteristics of Reusable Launch Vehicles
K. Tadakuma, Y. Tani, S. Aso
20163 citations Open access
Semantic Scholar
Morphing flap concept to reduce the flap side edge noise for aircraft wing slotted flaps
Y. Tani, Y. Yamashita, Kazuma Miyazaki, S. Aso +2 more
20143 citations
Semantic Scholar
Numerical Analysis of the Piston Motion in a Free Piston Driver
M. Mizoguchi, S. Aso
20073 citations Open access
Semantic Scholar
Numerical study on diaphragm rupture for performance improvement of a free piston shock tunnel
M. Mizoguchi, S. Aso
20063 citations
Semantic Scholar
An experimental study on shortening of ddt distance for pulse detonation engines
Ryuji Nakawatase, H. Miyazawa, S. Aso, Y. Tani
20063 citations
Semantic Scholar
A Study on O/F Shift of Aft Counter-Swirl Oxidizer Injection with Multi-Section Swirl Injection Method for Hybrid Rocket
Shohei Saiga, Atsushi Shirahama, S. Aso, Y. Tani +1 more
2019AIAA Scitech 2019 Forum2 citations
Semantic Scholar
Feasibility study on shared design of hypersonic transport and booster of TSTO for reduction of development cost
S. Aso, Y. Tani, T. Hirayama
20182 citations
Semantic Scholar
Schlieren visualization technique for high-enthalpy and low-density flow with LED light source
Naoki Morimoto, Jun Yamashita, Akihiko Tabata, S. Aso +1 more
20162 citations
Semantic Scholar
An expedient for alleviating aerodynamic heating and drag on capsule forward heat shield
Naoki Morimoto, Jun Yamashita, S. Aso, Y. Tani
20152 citations
Semantic Scholar
Preliminary Design of Winged Experimental Rocket by University Consortium
M. Wakita, K. Yonemoto, T. Akiyama, S. Aso +2 more
20092 citations Open access
Semantic Scholar
Influence of Coolant Gas Properties on Film Cooling Effectiveness in High Enthalpy Flows
M. Mizoguchi, S. Aso, Y. Tani
20092 citations
Semantic Scholar
Experimental study of fuselage effects on the aerodynamic performances of Reusable Launch Vehicle (RLV)
Takuro Ishida, S. Aso, Y. Tani, K. Tadakuma +1 more
20062 citations
Semantic Scholar
Lift augmentation by lateral blowing for RLVs with various fuselage-cross sections
K. Tadakuma, S. Aso, Takuro Ishida, Y. Tani +1 more
20062 citations
Semantic Scholar
Lateral Blowing for Aerodynamic Performance Improvement of Wing -Body -Configuration RLV
K. Tadakuma, S. Aso, Y. Tani
20052 citations
Semantic Scholar
Improvement of aerodynamic performances for reusable launch vehicles using the lateral blowing
K. Tadakuma, S. Aso, Y. Tani
20052 citations
Semantic Scholar

Frequent co-authors

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