Shigeru ASO

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Name
Shigeru ASO
E-mail
asokurume-it.ac.jp
Affiliation
Kurume Institute of Technology
Section
Faculty of Engineering Department of Transport Mechanical Engineering

Research Areas

 
 

Academic & Professional Experience

 
Apr 2019
 - 
Today
Distinguished Professor, Faculty of Engieering Department of Transport mechanical Engieering, Kurume Institute of Technology
 
Apr 1999
 - 
Mar 2019
Professor, Faculty of Engineerig Department of Aeronautics and Astronautics, Kyushu University
 

Published Papers

 
A Study of Multi-Section Swirl Injection Method Hybrid Rocket for Practical Application
Shohei Saiga , Atsushi Shirahama , Shigeru Aso , Yasuhiro Tani and Ryohei Arakawa and Toru Shimada
Proceedings of 2019 AIAA SciTech Forum, AIAA Paper 2019-1233, January 7-11, 2019,San Diego, CA, U.S.A.   2019(1233)    Jan 2019   [Refereed]
An Experimental Study on Passive Ventilation Wing with Porous Surfaces for Gust Load Alleviation
Shuhei Seki, Yasuhiro Tani and Shigeru Aso
Proceedings of 2019 AIAA SciTech Forum, AIAA Paper 2019-1105, January 7-11, 2019,San Diego, CA, U.S.A.   2019(1105)    Jan 2019   [Refereed]
An Experimental Study on Multistage Outrunner Motor Propeller System for Electric Airplanes
Y. Tani, A. Yasuda, S. Aso
Proceedings of 2019 AIAA SciTech Forum, AIAA Paper 2019-1330, January 7-11, 2019,San Diego, CA, U.S.A.   2019(1330)    Jan 2019   [Refereed]
Hybrid Rocket Firing Experiments at Various Axial?Tangential Oxidizer-Flow-Rate Ratios
Kohei Ozawa, Koki Kitagawa, Shigeru Aso and Toru Shimada
Journal of Propulsion and Power   35(1) 94-108   2019   [Refereed]
An Innovative Thermal Protection System with Opposing Jet through Extended Nozzle and Film Cooling for Reusable Launch Vehicles
Shigeru ASO and Yasuhiro Tani
Proceedings of 69th International Astronautical Congress, held at Bremen, Germany, 1-5 Oct. 2018, IAC-18-D2.5.5      Oct 2018   [Refereed]
A Study on Throttling, Anti-O/F Shift Operation and LOX Vaporization for Hybrid Rocket Engine with Multi-Section Swirl Injection Method
Shigeru ASO, Yasuhiro Tani, Shohei Saiga, Ryohei Arakawa, Atsushi Shirahamae and Toru Shimada
Proceedings of 69th International Astronautical Congress, held at Bremen, Germany, 1-5 Oct. 2018, IAC-18-C4.2.7      Oct 2018   [Refereed]
A Study on High Performance Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Space Propulsion System
Shigeru Aso, Yasuhiro Tani, Tani Shohei Saiga, Ryohei Arakawa, Toru Shimada
Proceedings of 2018 AIAA SciTech Forum,AIAA Paper 2018-1415, January 8-11, 2018,Kissimmee, FL,U.S.A.   2018(1415)    Jan 2018   [Refereed]
Feasibility Study on Shared Design of Hypersonic Transport and Booster of TSTO for Reduction of Development Cost
Shigeru Aso, Yasuhiro Tani and Takaaki Hirayama
Proceedings of 2018 AIAA SciTech Forum,AIAA Paper 2018-0278, January 8-11, 2018,Kissimmee, FL,U.S.A.   2018(278)    Jan 2018   [Refereed]
An Experimental Study on Gust Load Alleviation using Passive Vetilation Wing Concepy
Y. Tani, S. Seki and S. Aso
Proceedings of 2018 AIAA SciTech Forum, AIAA Paper 2018-1794, January 8-11, 2018,Kissimmee, FL,U.S.A.   2018(1794)    Jan 2018   [Refereed]
PASSIVE VENTILATION FLOW CONTROL FOR AIRCRAFT GUST LOAD ALLEVIATION
Y. Tani, S. Seki, S. Aso
31st ICAS Congress, held at Belo Horizonte, Brazil, on September 09-14,2018,ICAS 2018-7.1.2      2018   [Refereed]
An Experimental Study on Effect of Surface Properties on Aircraft Aeroacoustic Noise Reduction
Takuya Hirayama, Yasuhiro Tani, Shigeru Aso, Kazunori Mitsuo,Hiroki Ura, Takeshi Ito
Proceedings of 9th Kyushu University-KAIST Workshop on Aerospace Engineering, held at Fukuoka,Japan on Dec. 7-9, 2017.      Dec 2017   [Refereed]
Development of Subsystems of Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Practical Application
Shigeru Aso, Yasuhiro Tani, Shohei Saiga, Ryohei Arakawa, Masato Yamashita,Kazuya Komori, Tomohiro Yamasaki and Toru Shimada
Fourteenth International Conference on Flow dynamics, S8-12, held at Sendai International Center, Japan on Nov. 1-3, 2017      Nov 2017   [Refereed]
Throttling Capability and LOX Vaporization for Hybrid Rocket Engine with Multi-Section Swirl Injection Method
Shigeru Aso, Yasuhiro Tani, Masato Yamashita, Kazuya Komori, Tomohiro Yamasaki, Shohei Saiga, Ryohei Arakawa and Toru Shimada
68th International Astronautical Congress, IAC2017-C4.2.10, held on Sept. 25-29, 2017, at Adelaide, Australia      Sep 2017   [Refereed]
Flight Trajectory Analysis on Advanced Morphing Space Transportation System for Wider CrossRange and Down Range with Trimmed Flight
Shigeru Aso, Yasuhiro Tani , Kenta Shiomi
68th International Astronautical Congress, IAC2017-D2.IP.12, held on Sept. 25-29,2017, at Adelaide, Australia      Sep 2017   [Refereed]
Conceptual Design Investigation and Aerodynamic Study for Hypersonic Vehicle Baseline Configuration both for TSTO and HST
Takaaki Hirayama, Yasuhiro Tani and Shigeru Aso
31st ISTS, 26th ISSFD & 8th NSAT、2017-o-3-10 (平成29年6月)      Jun 2017   [Refereed]
A Study on Module-Type Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Optimum Combustion and Thrust Control
Shigeru Aso, Yasuhiro Tani, Masato Yamashita, Kazuya Komori, Tomohiro Yamasaki and Toru Shimada
31st ISTS, 26th ISSFD & 8th NSAT、2017-o-5-10      2017   [Refereed]
Development of Module-Type Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Optimum Combustion
Shigeru Aso, Yasuhiro Tani, Masato Yamashita, Kazuya. Komori, Tomohiro. Yamasaki, and Toru Shimada
Proceedings of 13th International Conference on Flow Dynamics, Oct. 10-12, 2016, Sendai,Japan (2016)      Oct 2016   [Refereed]
A Study on Advanced Morphing Space Transportation System for Wider Cross Range and Down Range
Kenta Shiomi, Shigeru Aso, Yasuhiro Tani
8th KAIST-Kyushu Univ. Symposium on Aerospace Engineering, held at KAIST、Daejeon, Korea,on October 13-15, 2016.      Oct 2016   [Refereed]
逆噴射ジェットによる高エンタルピー流中での空力加熱防御
森本直紀,山下 純,田畑明彦,麻生 茂,谷 泰寛
航空宇宙技術   15 33-42   Apr 2016   [Refereed]
Schlieren Visualization Technique for High-Enthalpy and Low-Density Flow with LED Light Source
Naoki Morimoto, Jun Yamashita, Akihiko Tabata, Shigeru Aso, and Yasuhiro Tani
Proc. 54th AIAA Aerospace Sciences Meeting, AIAA Paper 2016-1070 (2016).   2016(1070)    2016   [Refereed]
Static Burning Tests on a Bread Board Model of Altering-intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine
Kohei Ozawa, Tomoaki Usuki, Genki Mishima, Koki Kitagawa, Masato Yamashita, Masato Mizuchi,Shigeru Aso, Yasuhiro Tani, Yutaka Wada, and Toru Shimada
Proc. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, AIAA Propulsion and Energy Forum,AIAA Paper 2016-4964 (2016).   2016(4964)    2016   [Refereed]
An Experimental Study and Flight Trajectory Analysis on Advanced Morphing Space Transportation System for Wider Cross range and Down Range
Shigeru Aso, Yasuhiro Tani, Kenta Shiomi
Proceedings of 67th International Astronautical Congress, IAC-16,D2.5 (2016)      2016   [Refereed]
Development of Module-Type Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Flight Experiments, Proceedings of 67th International Astronautical Congress, IAC-16-C4.2.11 (2016)
Shigeru Aso, Yasuhiro Tani, Masato Mizuchi, Masato Yamashita, Koki Katakami, Yudai Maji and Toru Shimada
   2016   [Refereed]
Aerodynamic Study of Morphing Fully Reusable Launch Vehicle for Wider Cross Range and Down Range
Kenta Shiomi, Yasuhiro Tani and Shigeru Aso
7th Kyushu University-KAIST Symposium on Aerospace Engineering, held on December 10-12,2015 atKyushu University, Fukuoka, Japan(2015).      Dec 2015   [Refereed]
Experimental Investigation of Producing Hypersonic Test Gas Flow with Detonation Driven Expansion Tube
Shigeru Aso, Shiki Kitajima, Ryo Ikehara, Tadashi Jinnouchi, Naoki Morimoto, Yasuhiro Tani
Proc. 30th International Symposium on Space Technology and Sciences, ISTS 2015-a-27 (2015), held at Kobe-Hyogo, Japan, on July 4-10, 2015.      Jul 2015   [Refereed]
Numerical Study of Opposing Jet through Extended Nozzle in Hypersonic Flow
Jun Yamashita, Naoki Morimoto, Shigeru Aso, and Yasuhiro Tani
Proc. 30th International Symposium on Space Technology and Sciences, ISTS 2015-e-53(2015), held at Kobe-Hyogo, Japan, on July 4-10, 2015.      Jul 2015   [Refereed]
High Accuracy Piston Motion Estimation in Free-Piston Shock Tunnel
Naoki Morimoto, Akihiko Tabata, Jun Yamashita, Shigeru Aso, and Yasuhiro Tani
Proc.30th International Symposium on Space Technology and Sciences, ISTS 2015-e-62(2015), held at Kobe-Hyogo, Japan, on July 4-10, 2015.      Jul 2015   [Refereed]
Feasibility Study on Advanced Morphing Space Transportation System with Concept for Wider Cross Range and Down Range
Shigeru Aso and Yasuhiro Tani
Proc.30th International Symposium on Space Technology and Sciences, ISTS 2015-o-1-11(2015), held at Kobe-Hyogo, Japan, on July 4-10, 2015.      Jul 2015   [Refereed]
Ten Years of the Tanegashima Rocket Contest for Development of Young Generation in Space Engineering
Shigeru ASO, Hiroshi HIRAYAMA, Kazuhiko MORISHITA
Proc.30th International Symposium on Space Technology and Sciences, ISTS 2015-u-06(2015), held at Kobe-Hyogo, Japan, on July 4-10, 2015.      Jul 2015   [Refereed]
Development and Performance Verification of Ground Testing Device for Attitude Control of Micro satellite
Hiroshi Hirayama, Abdouallah Ramil, Shigeru Aso and Yasuhiro Tani
Proc.30th International Symposium on Space Technology and Sciences, ISTS 2015-f-94p(2015), held at Kobe-Hyogo, Japan, on July 4-10, 2015.      Jul 2015   [Refereed]
Study of Module Type Hybrid Rocket Engine with Multi-Section Swirl Injection Method, Proceedings of 30th International Symposium on Space Technology and Science
Masato Mizuchi, Kengo Ohe, Hiroshi Tada, Masato Yamashita, Shigeru Aso, Yasuhiro Tani and Toru Shimada
2015-a-19, Kobe, July 7-10, 2015, Kobe      Jul 2015   [Refereed]
An Expedient for Alleviating Aerodynamic Heating and Drag on Capsule Forward Heat Shield
Naoki Morimoto, Jun Yamashita, Shigeru Aso, and Yasuhiro Tani
53th AIAA Aerospace Sciences Meeting (SciTech 2015), AIAA-2015-2080, 5-9 January, 2015,KISSIMMEE, FL (2015).   2015(2080)    Jan 2015   [Refereed]
Experimental Investigation of Producing Hypersonic Test Gas Flow with Detonation Driven Expansion Tube
Shigeru Aso, Shiki Kitajima, Ryo Ikehara, Tadashi Jinnouchi, Naoki Morimoto, and Yasuhiro Tani
Proc. 30th International Symposium on Space Technology and Sciences, ISTS 2015-a-27(2015).      2015   [Refereed]
An Expedient for Alleviating Aerodynamic Heating and Drag on Capsule Forward Heat Shield
Naoki Morimoto, Jun Yamashita, Shigeru Aso and Yasuhiro Tani
Proc. 53rd AIAA Aerospace Sciences Meeting, AIAA SciTech2015, AIAA Paper 2015-2080(2015).   2015(2080)    2015   [Refereed]
Development of High Performance Hybrid Rocket Engine with Multi-Section Swirl InjectionMethod through Combustion Visualization and Various Injection Modification
Shigeru Aso, Yasuhiro Tani, Kengo Ohe, Hiroshi Tada, Masato Mizuchi, Masato Yamashita,Toru Shimada
Eleventh International Conference on Fluid Dynamics, ICFD2014, OS8-12,held on Oct.8-11,2014at Sendai, Japan (2014).      Oct 2014   [Refereed]
Aerodynamic Noise Reduction for High Lift Devices using Morphing Flap Concept
Yasuhiro TANI, Kazuma MIYAZAKI, Shigeru ASO, Hiroki URA and Takeshi ITO
29th Congress of the International Council of Aeronautical Sciences, ICAS2014-4.8.3,7-12 Sep. 2014, St. Petersburg, Russia (2014).      Sep 2014   [Refereed]
Morphing Flap Concept to Reduce the Flap Side Edge Noise for Aircraft Wing Slotted Flaps
Yasuhiro Tani, Yuya Yamashita, Kazuma Miyazaki, Shigeru Aso, Hiroki Ura and Takeshi Ito
AIAA Science and Technology Forum and Exposition 2014: 52nd Aerospace Sciences Meeting, AIAA-2014-0019、 Jan 13, 2014   2014(19)    Jan 2014   [Refereed]
Reduction of Aerodynamic Heating with the Opposing Jet from Extended Nozzle in High Enthalpy Flow
Naoki Morimoto, Jang Yeol Yoon, Shigeru Aso and Yasuhiro Tani Hiroshi Tada, Shigeru Aso, Yasuhiro Tani, Sho Ohyama, Kentaro Araki, Kengo Ohe, Masato Mizuchi and Toru Shimada: Visualization of Flames in Combustion Chamber of Hybrid Rocket Engine with Multi-Section Swirl Injection Method, Proceedings of 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA Paper 2014-3850 (2014)
AIAA Science and Technology Forum and Exposition 2014: 52nd Aerospace Sciences Meeting, AIAA-2014-0705、Jan 14, 2014   2014(705)    Jan 2014   [Refereed]
Visualization of Flames in Combustion Chamber of Hybrid Rocket Engine with Multi-Section Swirl Injection Method
Hiroshi Tada, Shigeru Aso, Yasuhiro Tani, Sho Ohyama, Kentaro Araki, Kengo Ohe, Masato Mizuchi and Toru Shimada
Proceedings of 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA Paper 2014-3850 (2014)   2014(3850)    2014   [Refereed]
Study on Hybrid Rocket with Multi-Section Swirl Injection Method toward Flight Experiments of Subscale Space Plane
Kengo Ohe, Masato Mizuchi, Shigeru Aso, and Yasuhiro Tani, Sho Ohyama, Kentaro Araki, Hiroshi Tada and Toru Shimada
Proceedings of 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA Paper 2014-3954 (2014)   2014(3954)    2014   [Refereed]
Reduction of Aerodynamic Heating and Drag with Opposing Jet through Extended Nozzle in High Enthalpy Flow
Naoki Morimoto, Shigeru Aso, and Yasuhiro Tani
Proc. 29th Congress of the International Council of the Aeronautical Sciences,ICAS2014-P2.3.2. (2014).      2014   [Refereed]
Aerodynamic Study of Advanced Space Transportation System with Morphing Concept for Wider Cross Range and Down Range
Shigeru Aso, Yasuhiro Tani and Kosuke Miyahara
Proceedings of 65th International Astronautical Congress, IAC-14,D2.P,11 (2014)      2014   [Refereed]
Development of High Performance Hybrid Rocket Engine with Multi-Section Swirl Injection Method for Space Propulsion System
Kengo Ohe, Shigeru Aso, Yasuhiro Tani, Sho Ohyama, Kentaro Araki, Hiroshi Tada, Masato Mizuchi and Toru Shimada
Proceedings of 65th International Astronautical Congress, IAC-14,C4,2.8 (2014)      2014   [Refereed]
Aerodynamic Noise Reduction for High Lift Devices using Morphing Flap Concept
Yasuhiro TANI, Kazuma MIYAZAKI, Shigeru ASO, Hiroki URA and Takeshi ITO
Proceedings of29th Congress of the International Council of Aeronautical Sciences,ICAS2014-4.8.3 (2014).      2014   [Refereed]
衝撃波干渉低減を考慮したTSTO型宇宙往還機の母機形状に関する実験的研究
植松太郎,麻生 茂,谷 泰寛
航空宇宙技術   12 89-97   Dec 2013   [Refereed]
A Study on Hybrid Rocket Engines with Multi-Section Swirl Injection Method for Low Cost and High Performance Space Propulsion System
Shigeru Aso, Yasuhiro Tani, Sho Ohyama, Kentaro Araki, Kengo Ohe, Hiroshi Tada, Masato Mizuchi and Toru Shimada
The 2013 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2013), Nov.20-23, 2013, Takamatsu, Japan      Nov 2013   [Refereed]
Aircraft Design and Feasibility Study on Light Electric Plane
Masahiro Sakamoto , Shigeru Aso and Yasuhiro Tan
The 2013 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2013), Nov.20-23, 2013, Takamatsu, Japan      Nov 2013   [Refereed]
Development of GOX Hybrid Rocket Test Engine Facility in Hybrid Rocket Research Working Group
Koki Kitagawa, Toru Shimada, Keiichi Hori, Toshiaki Takemae, Noriko Shiraishi, Toshio Tomizawa, Naohiro Suzuki, Tsuyoshi Yagishita, Nobuyuki Oshima, Harunori Nagata, MasashiWakita, Kazuhisa Chiba, Keisuke Sawada, Hiroki Nagai, YutakaWada, Saburo Yuasa, Takashi Sakurai, Masahiro Kanazaki, Ichiro Nakagawa, Takakazu Morita, Masaki Nakamiya, Shigeru Aso, Yasuhiro Tani, Nobuyuki Tsuboi
Tenth International Conference on Flow Dynamics (ICFD2013), Nov.25-27, 2013.      Nov 2013   [Refereed]
Enhancement of Higher Regression Rate and Combustion Efficiency of Hybrid Rocket Engines with Multi-Section Swirl Injection Method
Shigeru Aso, Yasuhiro Tani, Sho Ohyama, Kentaro Araki, Kengo Ohe, Hiroshi Tada, Masato Mizuchi, Hiroshi Hirayama and Toru Shimada2
Tenth International Conference on Flow Dynamics (ICFD2013), Nov.25-27, 2013.      Nov 2013   [Refereed]
Development of University Ground Station for Nano Satellite Operation
Shigeru Aso, Kiyotaka Fujisaki, Hiroshi Hirayama, Kazuhiko Morishita, Tsutomu Tokifuji, Naomi Kurahara, Yoshihiro Tsuruda
5th Nano-Satellite Symposium, Nov. 21, 2013.      Nov 2013   [Refereed]
Performance Evaluation of Ground Station in Kyushu University
Hiroshi Hirayama, Kazuhiko Morishita, Kiyotaka Fujisaki, Shigeru Aso, Tsutomu Tokifuji, Naomi Kurahara
5th Nano-Satellite Symposium, Nov. 22, 2013.      Nov 2013   [Refereed]
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, S. Aso, and Y. Tani and Toru SHIMADA
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit and 11th International Energy Conversion Engineering Conference, July 14-17, 2013, San Jose. AIAA-2013-4040   2013(4040)    Jul 2013   [Refereed]
A Study on Performance Improvement of Paraffin Fueled Hybrid Rocket Engines with Multi-Section Swirl Injection Method
Kentaro Araki, Yoshihide Hirata, Sho Oyama, Kengo Ohe, Shigeru Aso, Yasuhiro Tani and Toru Shimada
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit and 11th International Energy Conversion Engineering Conference, July 14-17, 2013, San Jose. AIAA 2013-3634   2013(3634)    Jul 2013   [Refereed]
Increase of Fuel Regression Rate with Multi-section Swirl Injection Method in High Density Polyethylene Fueled Hybrid Rocket Motor
Sho Ohyama, Yoshihide Hirata, Kentaro Araki, Kengo Ohe, Shigeru Aso, Yasuhiro Tani,Toru Shimada
29th International Symposium on Space Technology and Science, 2013-a-28, June 2-9, 2013,Nagoya      Jun 2013   [Refereed]
Effects of Multi-Section Injection Method with and without Swirl on Regression Rate forParaffin Fueled Hybrid Rocket Engines
Kentaro Araki, Yoshihide Hirata, Sho Ohyama, Kengo Ohe, Shigeru Aso, Yasuhiro Tani,Toru Shimada
29th International Symposium on Space Technology and Science, 2013-a-29, June 2-9, 2013,Nagoya      Jun 2013   [Refereed]
Effect of the Opposing Jet on Reduction of Aerodynamic Heating of Pitched Blunt Body
Naoki Morimoto, Jang Yeol Yoon, Shigeru Aso, Yasuhiro Tani
29th International Symposium on Space Technology and Science, 2013-e-05, June 2-9, 2013, Nagoya      Jun 2013   [Refereed]
Development of University Ground Station for Nano Satellite Operation
Shigeru Aso, Kiyotaka Fujisaki, Kazuhiko Morishita, Tsutomu Tokifuji, Naomi Kurahara
29th International Symposium on Space Technology and Science, 2013-f-45, June 2-9, 2013, Nagoya      Jun 2013   [Refereed]
Aerodynamic Study on Morphing Space Transportation System
Kosuke MIYAHARA, Shigeru ASO, Yasuhiro TANI, Kyosuke YANASE and Yoshifumi INATANI
29th International Symposium on Space Technology and Science, 2013-g-03, June 2-9, 2013, Nagoya      Jun 2013   [Refereed]
Improvement of Detonation-Driven Expansion Tube by Changing H2/O2 Mixture Ratio of Detonation Driver
Tadashi JINNOUCHI, Shigeru ASO, Yasuhiro TANI
2012 Asia-Pacific International Symposium on Aerospace Technology (APISAT-2012), 1.7.2, November 14, 2012      Nov 2012   [Refereed]
A Development of High Enthalpy Facility of Air and Hydrogen with Detonation-Driven Expansion Tube
Tadashi JINNOUCHI, Shigeru ASO, Yasuhiro TANI
2012 Asia-Pacific International Symposium on Aerospace Technology (APISAT-2012), 1.7.3, November 14, 2012      Nov 2012   [Refereed]
New Ground Station Development at Kyushu University for Nano Satellite Operation
Shigeru ASO, Kiyotaka FUJISAKI, Tsutomu TOKIFUJI, Kazuhiko MORISHITA, Naomi KURAHARA and Yoshihiro TSURUDA
63rd International Astronautical Congress, IAC-12-B4.3.6, Oct. 2012      Oct 2012   [Refereed]
Performance Advancement of Hybrid Rocket Engine through Higher Regression Rate and Combustion Efficiency with Multi-section Swirl Injection Method
Yoshihide HIRATA, Sho OHYAMA, Shigeru ASO, Yasuhiro TANI, Toru SHIMADA
63rd International Astronautical Congress, IAC-12-C4.2.26, Oct. 2012      Oct 2012   [Refereed]
An Experimental Study on Highly Efficient DDT Enhancement Device for PDE
Ryuji NAKAWATASE, Kazunari TSURU, Shigeru ASO, Yasuhiro TANI
63rd International Astronautical Congress, IAC-12-C4.5.7, October, 2012      Oct 2012   [Refereed]
Experimental Study of the Morphing Flap as a Low Noise High Lift Device for Aircraft Wing
Yasuhiro TANI, Yoshiyuki MATSUDA, Akira DOI, Yuya YAMASHITA, Shigeru ASO and Takeshi ITO
28th International Congress of the Aeronautical Sciences, ICAS2012-9.11.3, 24-27 September, 2012      Sep 2012   [Refereed]
Development of Hybrid Rocket Engines with Multi-Section Swirl Injection Method for Higher Regression Rate and Combustion Efficiency
Shigeru ASO, Yasuhiro TANI, Yoshihide HIRATA, Sho OHYAMA, Kentaro ARAKI, Kengo OHE and Toru SHIMADA
ICFD2012, Sept.19-21, 2012, Sendai, Japan      Sep 2012   [Refereed]
A Study of Hybrid Rockets with Multi-Section Swirl Injection Method
Sho OHYAMA, Shigeru ASO, Yoshihide HIRATA, Kentaro ARAKI, Kengo OHE, Yasuhiro TANI, Toru SHIMADA
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2012-3905, July, 2012   2012(3905)    Jul 2012   [Refereed]
Supersonic Flight Separation Simulation for TSTO Launch Vehicles Considering Shock Wave Interaction Reduction
Taro UEMATSU Shigeru ASO and Yasuhiro TANI
Proceedings of 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA-2012-0253, January, 2012   2012(253)    Jan 2012   [Refereed]
Development of Challenging Technology of Novel Structure System and Non-Explosive, Low-Cost, Low-Vibration Separation Device of Nano Satellite QSAT-EOS
Shigeru ASO, Testuo YASAKA, Shunsuke ONISHI, Osamu URUMA, Seiya NAGANO and Tokuo KAWASHIMA
IAC-12-B4.6B.2, 2012.10.4      2012   [Refereed]
Research and Development of Nano-Satellite QSAT-EOS for Earth Observation System Demonstrator in Kyushu University
Shigeru Aso, Tetsuo Yasaka, Yasuhiro Tani, Toshiya Hanada, Haruhiko Ohta, Masahiko Murozono, Masatoshi Omura, Yoshihiro Tsuruda , Shunsuke Onishi
Proceedings of 5th Kyushu Univ.-KAIST Symposium on Aerospace Engineering, held at Fukuoka City, Fukuoka, Japan, on November 24-26, 2011      Nov 2011   [Refereed]
Reduction of Aerodynamic Heating by Opposing Jet
Kouyuu Hamasaki, Shigeru Aso, and Yasuhiro Tani
Proceedings of 5th Kyushu Univ.-KAIST Symposium on Aerospace Engineering, held at Fukuoka City, Fukuoka, Japan, on November 24-26, 2011      Nov 2011   [Refereed]
Experiment to Estimate Aerodynamic Characteristics of FRLV
Yuta Fujii, Shigeru Aso, and Yasuhiro Tani
Proceedings of 5th Kyushu Univ.-KAIST Symposium on Aerospace Engineering, held at Fukuoka City, Fukuoka, Japan, on November 24-26, 2011      Nov 2011   [Refereed]
Improvement of Regression Rate and Combustion Efficiency of High Density Polyethylene Fuel and Paraffin Fuel of Hybrid Rockets with Multi-Section Swirl Injection Method
Yoshihide HIRATA, Shigeru ASO, Takahiro HAYASHIDA, Ryuji NAKAWATASE, Yasuhiro TANI, Kazuhiko MORISHITA and Tohru SHIMADA
Proceedings of 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2011-5907, August 2011      Aug 2011   [Refereed]
Thermal and Structural Design of QSAT-EOS
Shunsuke Onishi, Sigeru Aso, Haruhiko Ohta, Masahiko Murozono, Tetsuo Yasaka
Proccedings of International Symposium on Space Technology and Science, held at Ginowan City, Okinawa, Japan, on June 5-12, 2011, ISTS-2011-f-29      Jun 2011   [Refereed]
QSAT-EOS: 50kg-class Small Satellite for Earth Observation System Demonstration
Shigeru Aso, Tetsuo Yasaka, Yasuhiro Tani, Toshiya Hanada, Masahiko Murozono, Masatoshi Omura, Yoshihiro Tsuruda , Shunsuke Onishi, Kohei Arai, Mengu Cho, Masanori Nishio
Proccedings of International Symposium on Space Technology and Science, held at Ginowan City, Okinawa, Japan, on June 5-12, 2011, ISTS-2011-f-28      Jun 2011   [Refereed]
New Needs of Low-Cost Launcher with Hybrid Rocket Engine for Micro-Satellite and Recent Topic on Increase of Combustion Efficiency with Multi-Swirl Injection
Shigeru Aso, Yasuhiro Tani, Yoshihide Hirata, Takahiro Hayashida, Ryuji Nakawatase, Toru Shimada
Proccedings of International Symposium on Space Technology and Science, held at Ginowan City, Okinawa, Japan, on June 5-12, 2011, ISTS-2011-o-1-11v      Jun 2011   [Refereed]
New Ground Station Development at Kyushu University for Nano Satellite Operation
Yoshihiro TSURUDA, Shigeru ASO, Tsutomu Tokihuji, Naomi Kurahara and Shinichi NAKASUKA
Proccedings of International Symposium on Space Technology and Science, held at Ginowan City, Okinawa, Japan, on June 5-12, 2011, ISTS-2011-f-36      Jun 2011   [Refereed]
Improvement of Regression Rate and Combustion Efficiency of Paraffin Fuel Hybrid Rockets with Multi-section Swirl Injection
Yoshihide Hirata, Takahiro Hayashida, Ryuji Nakawatase, Shigeru Aso, Yasuhiro Tani, Kazuhiko Morishita
Proccedings of International Symposium on Space Technology and Science, held at Ginowan City, Okinawa, Japan, on June 5-12, 2011, ISTS-2011-a-50      Jun 2011   [Refereed]
Improvement of Combustion Efficiency of High Density Polyethylene Fuel Hybrid Rockets with Multi-Section Swirl Injection
Takahiro Hayashida, Yoshihide Hirata, Ryuji Nakawatase, Shigeru Aso, Yasuhiro Tani,Kazuhiko Morishita
Proccedings of International Symposium on Space Technology and Science, held at Ginowan City, Okinawa, Japan, on June 5-12, 2011, ISTS-2011-a-03      Jun 2011   [Refereed]
Enhancement of Multi-Section Swirl Injection Method for Increase of Regression Rate and Combustion Efficiency of Hybrid Rockets
Shigeru Aso, Yoshihide Hirata, Yasuhiro Tani, Takahiro Hayashida and Ryuji Nakawatase
Proceedings of Eighth International Conference on Flow Dynamics, held at Sendai, Miyagi, Japan, on November 9-11, 2011,      Jun 2011   [Refereed]
Enhancement of Aerodynamic Heating Reduction in High Enthalpy Flows with Opposing Jet
Takashige IMOTO, Hisashi OKABE, Shigeru ASO and Yasuhiro TANI
Proceedings of 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA-2011-346, January, 2011   2011(346)    Jan 2011   [Refereed]
Effects of the Injection of Coolant gas on the Reduction of Aerodynamic Heating in High Enthalpy Flow
Shigeru Aso, Takashige Imoto, Hisashi Okabe, and Yasuhiro Tani
AIAA Paper 2011-0346, 2011.   2011(346)    2011   [Refereed]
Aerodynamic Interference Reduction Method for Two-Stage Launch Vehicles Supersonic Separation
Taro Uematsu, Shigeru Aso, Yasuhiro Tani
AIAA Paper 2011-0389, 2011.   2011(389)    2011   [Refereed]
A Study on New Swirling Injection method for Polyethylene Fuel and Paraffin Fuel of Hybrid Rocket Engines
Shigeru ASO, Yasuhiro TANI, Wataru MITSUNAKA, Takafumi MATSUZAKI, Ryuji NAKAWATASE, Yoshihide HIRATA and Takahiro HAYASHIDA
Seventh International Conference on Flow Dynamics, GS1-16, November, 2010.      Nov 2010   [Refereed]
Remarkable Aerodynamic Performance of Triangle Cross Section Configuration for Fully RLV
Shigeru ASO, Takuro ISHIDA and Yasuhiro TANI
61st International Astronautical Congress 2010, IAC-10-D2-P01, September, 2010.      Sep 2010   [Refereed]
A Numerical Study on Reduction of Propellants for Reaction Control Systems with Improvement of jet Interaction
Yu ETOH, Shigeru ASO and Yasuhiro TANI
61st International Astronautical Congress 2010, IAC-10-D2-P02, September, 2010.      Sep 2010   [Refereed]
A New Challenge for Improvement of Recession Rate of High Density Polyethylene Fuel and Paraffin Fuel of Hybrid Rocket with Multi-Section Swirl Injection
Shigeru ASO, Takafumi MATSUZAKI, Wataru MITSUNAKA, Ryuji NAKAWATASE and Yasuhiro TANI
61st International Astronautical Congress 2010, IAC-10.C4.2.10, September 2010.      Sep 2010   [Refereed]
Reducing Aerodynamic Heating by the Opposing Jet in Supersonic and Hypersonic Flows
Isao TAMADA, Shigeru ASO and Yasuhiro TANI
Proceedings of 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA-2010-991, January, 2010.   2010(991)    Jan 2010   [Refereed]
A Proposal of New Fuselage Configurations for Realizing Reusable Launch Vehicles
Takuro ISHIDA, Shigeru ASO and Yasuhiro TANI
48th AIAA Aerospace Science Meeting and Exhibit, AIAA-2010-1045, in Orlando, Florida, U.S.A 4th-7th, Jan., 2010   2010(1045)    Jan 2010   [Refereed]
A study on supersonic mixing by circular nozzle with various injection angles for air breathing engine
S. Aso, K. Inoue, K. Yamaguchia and Y. Tania
Acta Astronautica   65(5ー6) 687-695   Oct 2009   [Refereed]
Aerodynamic Design and its Validation of an Open-type Engine Run-up Facility
M Kawai, K Nagai, S Aso
Proceedings of CEAS 2009 European Air and Space Conference, held on 26-29 October, 2009 at Manchester, UK      Oct 2009   [Refereed]
Reduction of Aerodynamic Interference for Separation of Two-Stage Reusable Launch Vehicles
Taro UEMATSU, Takuro ISHIDA, Shigeru ASO and Yasuhiro TANI
Proceedings of 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, AIAA 2009-1101, January, 2009.   2009(1101)    Jan 2009   [Refereed]
Influence of Coolant Gas Properties on Film Cooling Effectiveness in High Enthalpy Flows
Makoto MIZOGUCHI, Shigeru ASO and Yasuhiro TANI
Proceedings of 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, AIAA 2009-1034, January, 2009.   2009(1034)    Jan 2009   [Refereed]
A Study of Fuselage Configurations for Reusable Launch Vehicles
Takuro ISHIDA, Shigeru ASO, Yasuhiro TANI, Yoshifumi INATANI and Tomoko IRIKADO
Proceedings of 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, AIAA 2009-906, January, 2009.   2009(906)    Jan 2009   [Refereed]
The effect of diaphragm opening time on the feasibility of tuned operation in free pistonshock tunnels
Makoto Mizoguchi and Shigeru Aso
Shock Waves, Vol. 19 (2009)   337-347   2009   [Refereed]
An Experimental Study on the Improvement of Aerodynamic Characteristics of Lifting Body Configuration by Active Flow Control Method
Shigeki TSUCHIYA,Shigeru Aso, Yasuhiro Tani
Memoirs of the Engineering, Kyushu University   68(4) 175-192   Dec 2008   [Refereed]
Numerical Study on Supersonic Mixing Enhancement with a Ramp Injector and a Cavity
Fumihiko NISHIMOTO, Kohei YAMAGUCHI, Shigeru ASO and Yasuhiro TANI
Proceedings of 2008 KSAS-JSAS Joint Symposium on Aerospace Engineering,C4-3,November,2008      Nov 2008   [Refereed]
An Experimental Study on the Improvement of Aerodynamic Characteristics Using the Blowing for RLV
Shigeki TSUCHIYA, Shigeru ASO and Yasuhiro TANI
Proceedings of 2008 KSAS-JSAS Joint Symposium on Aerospace Engineering, A4-4, November,2008,Nov 20 -21, 2008 in Jeju Island, Korea      Nov 2008   [Refereed]
Supersonic Combustion Enhancement by Shock Wave Impingement for Scram-Jet Engine
Arif Nur Hakim, Shigeru Aso, Yasuhiro Tani
Proceedings of the 57th International Aeronautical Congress, IAC-08-C4.5.9, October, 2008      Oct 2008   [Refereed]
Fundamental Study on Pulse Detonation Engine with Liquid Fuel for Aerospace Propulsion System
Ryuji NAKAWATASE, Yoichiro NISHIMURA, Shigeru ASO and Yasuhiro TANI
Proceedings of the 57th International Aeronautical Congress, IAC-08-C4.5.14, October, 2008      Oct 2008   [Refereed]
AERODYNAMIC DESIGN AND ITS VALIDATION OF AN OPEN-TYPE ENGINE RUN-UP FACILITY
Masafumi KAWAI,Kiyoyuki NAGAI and Shigeru ASO
Proceedings of 26th Congress of International Council of the Aeronautical Sciences, ICAS 2008-4.5.3 , September, 2008      Oct 2008   [Refereed]

Misc

 
小型電動航空機の研究開発の試みと今後の発展性について
麻生 茂、谷 泰寛
日本航空宇宙学会誌   66(1) 18-24   Jan 2018   [Refereed]
Research and Development of 50kg-class Micro Satellite QSAT-EOS (Tsukushi) in Kyushu University
Shigeru ASO
1st International Workshop on SPACE SITUATIONAL AWARENESS, held at KAIST, Daejeon, Korea, on Dec. 6-8,2018. (Invited Paper)      2018   [Refereed][Invited]
High-Speed Flow Research at Kyushu University
Shigeru ASO
The 1st International Symposium on Hypersonics, held at KAIST, Daejeon, Korea, on Nov. 28-29,2016. (Invited Paper)      Nov 2016   [Refereed][Invited]
Research Activities on Hybrid Rocket Engine and Small Electric Plane
Shigeru ASO
8th KAIST-Kyushu Univ. Symposium on Aerospace Engineering, held at KAIST、Daejeon, Korea,on October 13-15, 2016.(Invited Paper)      Oct 2016   [Refereed][Invited]
Aircraft design and feasibility study on electric plane toward green flight technology
Shigeru Aso and Yasuhiro Tani
France-Japan Joint Forum on “Recent Advances in Aeronautics and Space: Smart and GreenTechnologies and Applications for the future”, held on June 12-13, 2014, at Toulouse, France.(Invited Paper)      Jun 2014   [Refereed][Invited]
リモートセンシング質問箱(第18回)超小型衛星の特徴や利点について
麻生 茂
日本リモートセンシング学会誌   34(1) 33-35   2014   [Refereed]
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, W. MORITA and K. TADAKUMA
34th AIAA Fluid Dynamics Conference and Exhibit, June 28- July 1, 2004, Portland, Oregon,U.S.A.AIAA Paper 2004-2536(invited paper)   2004(2536)    Jun 2004   [Refereed][Invited]
将来型航空機・宇宙機研究開発に関する世界の動向と日本の体制 日本の大学における取り組み
麻生 茂
機械の研究   56(1) 208-212   Jan 2004   [Refereed]
A Study on Active Flow Control for Next-Generation SST for Higher L/D
S. ASO, M. KAMISHITA, K. KARASHIMA and K. SATO
32nd AIAA Fluid Dynamics Conference and Exhibit, June 24-26, 2002, St. Louis, MI, U.S.A.,AIAA Paper 2002-2844 (invited paper)   2002(2844)    Jun 2002   [Refereed][Invited]
完全再使用宇宙往還機の空力加熱
麻生 茂
日本航空宇宙学会誌   49(570) 149-151   Jul 2001   [Refereed]
「高温反応性気体:実験と数値計算」報告
麻生 茂
日本航空宇宙学会誌   46(533) 320-322   Jun 1998   [Refereed]
円孔噴射による三次元超音速混合流の数値計算
山根善行、安藤安則、麻生 茂、坂田公夫
日本数値流体力学会誌   5(2) 62-65   Jan 1997   [Refereed]
衝撃波誘起非定常空力加熱現象の数値計算
麻生 茂
日本数値流体力学会誌   5(1) 22-27   Oct 1996   [Refereed]
種々の可視化法による衝撃波/乱流境界層干渉場の流れの可視化
麻生 茂、前川昌三、辛島桂一、佐藤 清
日本航空宇宙学会誌   44(509) 354-359   Jun 1996   [Refereed]
フリーピストン衝撃波管の作動特性
木原 尚、麻生 茂、西田迪雄
日本航空宇宙学会誌   43(499) 446-450   Aug 1995   [Refereed]
Unsteady Aerodynamic Heating Structure in Shock Wave Reflection Processes
Shigeru ASO
Proceedings of 1st Asian Computational Fluid Dynamics Conference, held at Hong Kong, on Jan. 16-19, 1995   51-59   Jan 1995   [Refereed]
スペースプレーンの衝撃波干渉問題の計測法について
麻生 茂
日本航空宇宙学会誌   42(482) 164-168   Mar 1994   [Refereed]
スクラムジェットのための超音速混合流の基礎研究
麻生 茂、安藤安則
日本流体力学会誌   13(1) 36-37   Feb 1994   [Refereed]
超音速流中の二次流のジェット干渉流れ場の数値流体力学によるアプローチ
安藤安則、麻生 茂
日本流体力学会誌   13(1) 1-2   Feb 1994   [Refereed]
スペースプレーンの空力加熱問題
麻生 茂
日本流体力学会誌   10(2) 152-154   Jun 1991   [Refereed]
極超音速流における空力加熱について
林 正徳、麻生 茂
日本航空宇宙学会誌   38(435) 178-186   Apr 1990   [Refereed]
渦:剥離渦研究の動向について
林 正徳、麻生 茂
日本航空宇宙学会誌   37(421) 54-60   Feb 1989   [Refereed]
パネル法と離散渦法を用いた剥離流の数値シミュレーション
林 正徳、麻生 茂
日本航空宇宙学会誌   34(390) 350-355   Jul 1986   [Refereed]
Surface Hot Film による剥離を伴う翼の可視化実験
林 正徳、桜井 晃、麻生 茂、大串良昭
日本航空宇宙学会誌   31(359) 690-695   Dec 1983   [Refereed]

Books etc

 
Hybrid Propulsion Technology Development in Japan for Economic Space Launch, Chemical Rocket Propulsion
Shimada, T., Yuasa, S., Nagata, H., Aso, S., Nakagawa, I., Sawada, K., Hori, K., Kanazaki, M., Chiba, K, Sakurai, T., Morita, T., Kitagawa, K., Wada, Y., Nakata, D., Motoe, M., Funami, Y., Ozawa, K., Usuki, T.
Springer   Aug 2017   ISBN:978-3-319-27748-6
Chemical Rocket Propulsion: A Comprehensive Survey of Energetic Materials, Springer International Publishing
分担執筆
Aug 2016   
圧縮性流体力学
麻生茂 川添博光 澤田惠介
丸善出版   Oct 2015   
風工学ハンドブック
分担執筆
朝倉書店   Apr 2007   
航空宇宙工学便覧(第3版)
分担執筆
丸善   Nov 2005   
ながれの辞典
分担執筆
丸善   Mar 2004   
流れの可視化
分担執筆
朝倉書店   Dec 1996   
衝撃波ハンドブック
分担執筆
SpringerJapan   Dec 1995   
Integral methods in science and engineering
分担執筆
LongmanScientific&Technical   Oct 1994   
翼理論
柘植俊一、麻生 茂 共訳(原著 R.T.Jones)
日刊工業新聞社   Nov 1993   
航空宇宙工学便覧(改訂版)
分担執筆
丸善   Sep 1992   
数値流体力学
分担執筆
東大出版会   Feb 1992   

Patents

 
特開昭60-201224 : 多層薄膜熱伝達ゲ-ジ
林 正徳、桜井 晃、麻生 茂