Search

Your search keyword '"Tanno, Hideyuki"' showing total 266 results
Start Over Author "Tanno, Hideyuki"

Refine your results

more »

more »

more »

more »
266 results on '"Tanno, Hideyuki"'

1. Hayabusa2 reentry and recovery operations of the sample return capsule

Author

Nakazawa, Satoru, primary, Kawahara, Kosuke, additional, Yamada, Tetsuya, additional, Fujita, Naoyuki, additional, Ishimaru, Takahiro, additional, Miura, Akira, additional, Ito, Taichi, additional, Hayashi, Daisuke, additional, Fujita, Kazuhisa, additional, Tanno, Hideyuki, additional, Sawada, Hirotaka, additional, Tanaka, Satoshi, additional, Kobiki, Noboru, additional, Saiki, Takanao, additional, and Tsuda, Yuichi, additional

Published
2022
Full Text
View/download PDF

2. Contributors

Author

Abe, Masanao, primary, Arakawa, Masahiko, additional, Bellerose, Julie, additional, Danno, Satoshi, additional, Farnocchia, Davide, additional, Fujii, Atsushi, additional, Fujita, Kazuhisa, additional, Fujita, Naoyuki, additional, Furukawa, Katsumi, additional, Goto, Daisuke, additional, Hayashi, Daisuke, additional, Hihara, Hiroki, additional, Hirabayashi, Masatoshi, additional, Hirose, Chikako, additional, Ho, Tra-Mi, additional, Honda, Rie, additional, Hosoda, Satoshi, additional, Ichikawa, Tsutomu, additional, Ikeda, Hitoshi, additional, Ishibashi, Ko, additional, Ishimaru, Takahiro, additional, Ito, Taichi, additional, Kadono, Toshihiko, additional, Kagawa, Hideshi, additional, Kameda, Shingo, additional, Kato, Takaaki, additional, Kawahara, Kosuke, additional, Kikuchi, Shota, additional, Kitazato, Kohei, additional, Kobiki, Noboru, additional, Kouyama, Toru, additional, Kushiki, Kenichi, additional, Maru, Yusuke, additional, Masuda, Tetsuya, additional, Matsuhisa, Takashi, additional, Matsuoka, Masatoshi, additional, Matsuoka, Moe, additional, Matsushima, Kota, additional, Michigami, Keisuke, additional, Mimasu, Yuya, additional, Miura, Akira, additional, Mori, Osamu, additional, Morota, Tomokatsu, additional, Moussi, Aurelie, additional, Nagata, Taiichi, additional, Nakatsuka, Junichi, additional, Nakazawa, Satoru, additional, Namiki, Noriyuki, additional, Nishiyama, Kazutaka, additional, Oda, Kenji, additional, Ogawa, Kazunori, additional, Ogawa, Naoko, additional, Ohnishi, Takafumi, additional, Okada, Tatsuaki, additional, Oki, Yusuke, additional, Ono, Go, additional, Oshima, Takeshi, additional, Saiki, Takanao, additional, Sakatani, Naoya, additional, Sano, Junpei, additional, Sawada, Hirotaka, additional, Sawai, Shujiro, additional, Shida, Maki, additional, Shimada, Daisuke, additional, Shimada, Takanobu, additional, Shirai, Kei, additional, Soldini, Stefania, additional, Sugita, Seiji, additional, Tachibana, Shogo, additional, Takami, Tsuyoshi, additional, Takei, Yuto, additional, Takeuchi, Hiroshi, additional, Tanaka, Satoshi, additional, Taniguchi, Sho, additional, Tanno, Hideyuki, additional, Tarzi, Zahi, additional, Tasker, Elizabeth, additional, Tatsumi, Eri, additional, Terui, Fuyuto, additional, Toda, Tomoaki, additional, Tsuda, Yuichi, additional, Tsukizaki, Ryudo, additional, Uo, Masashi, additional, Uramachi, Hikaru, additional, Van Wal, Stefaan, additional, Wada, Koji, additional, Watanabe, Sei-ichiro, additional, Yabuta, Hikaru, additional, Yamada, Manabu, additional, Yamada, Tetsuya, additional, Yamaguchi, Tomohiro, additional, Yasuda, Seiji, additional, Yokota, Yasuhiro, additional, Yoshikawa, Keisuke, additional, Yoshikawa, Kent, additional, Yoshikawa, Makoto, additional, and Yumoto, Koki, additional

Published
2022
Full Text
View/download PDF

9. Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes

Author

Radespiel, Rolf, Ali, Syed R. C, Bowersox, Rodney, Leidy, Andrew, Tanno, Hideyuki, Kirk, Lindsay C, and Reshotko, Eli

Subjects
Aerodynamics
Abstract

The present contribution reviews recent experimental results of roughness effects on boundary layer transition on capsule geometries with spherical windward geometries. Experiments in three wind tunnel facilities are considered. The ACE Tunnel of Texas AM University, USA, provided Mach 6 experiments with distributed roughness at relatively low Reynolds numbers, 2.5 · 10(exp 5) < Re(sub d) < 5 · 10(exp 5), with d denoting the capsule diameter. The observed boundary layer transition compared well with correlations based on transient growth theory, even though the roughness heights were in the order of boundary layer thickness. Larger Reynolds numbers, 1 · 10(exp 6) < Re(sub d) < 3·10(exp 6), could be assessed in the hypersonic Ludwieg tube, HLB, of TU Braunschweig, Germany. Transition is observed at rather low, subcritical roughness values in the order of 20 μm for a roughness patch placed about the geometric center of the capsule model. These experiments varied fluctuation levels of the freestream. The authors assume that the observed transitions that occur downstream of the subcritical roughness patch are due to freestream disturbances in the tunnel, which interact with small roughness heights. Additional experiments in the HLB facility with patches of larger roughness height support the relevance of transient growth theory for low-to-medium roughness heights, relative to boundary layer thickness. The effects of Reynolds numbers and total flow enthalpy on transition with isolated roughness were investigated in the HIEST facility of JAXA, Japan. Here, a model insert with roughness elements of varying height for tripping transition to turbulence was employed. The results are compared to known trip effectiveness correlations for isolated roughness. Overall, the transient growth correlation seems to represent roughness-induced transition behavior on the ACE and HLB entry capsule shapes with roughness over the entire capsule surface. These experiment are however for perfect gases. Comparable experiments on roughness induced transition in a high-enthalpy facility are still needed to confirm the validity of transient-growth correlation for vehicle design.

Published
2018
Full Text
View/download PDF

10. 高忠実な物理モデルによるリエントリ安全評価法LS-DARCの開発: 第2報 熱流束モデル検証プロセス

Author

FUJIMOTO, Keiichiro, NEGISHI, Hideyo, IIZUKA, Nobuyuki, TANNO, Hideyuki, SHIMIZU, Ryuzo, and OKITA, Koichi

Abstract

第9回スペースデブリワークショップ (2021年2月24-26日. 宇宙航空研究開発機構調布航空宇宙センター(JAXA)(CAC), オンライン会議), 調布市, 東京, The 9th Space Debris Workshop (February 24-26, 2021. Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)(CAC), Online meeting), Chofu, Tokyo, Japan, 宇宙開発はこの半世紀において科学や工学の両面において飛躍的な発展を遂げてきた．一方，宇宙開発を今後も持続可能なものにするためにはスペースデブリ問題の対策が重要である．本研究は新たなデブリ発生を抑える非デブリ化対策として，ロケット上段や宇宙機の大気圏突入後の溶融残存物による地上被害リスクの最小化を目指している．本研究では，とくに高忠実な物理モデルをベースとした複合物理連成解析法であるリエントリ安全評価法LS-DARC（Destructive Atmospheric Re-entry Code）の開発に取組んでいる．設計パラメータ変更による安全性向上度を定量的に分析できるようにすることで，a) 上流設計段階からの溶融促進設計，b) 認知学的な不確かさの低減による高精度なリスク評価を実現することが目的である．LS-DARCにより下図に示すようなロケット上段や衛星などの複雑形状に対して溶融残存物が生じるかどうかを評価することができるが，安全評価法として実用化するためには物理モデルの検証プロセスの確立が不可欠である．本報告ではとくに熱流束モデル検証方法を提案し，高エンタルピー風洞試験による検証データ取得をはじめとした検証状況について述べる．, Remarkable progress in space exploration both for science and engineering have been made in a half century. Space debris problem is a growing concern to be tackled internationally to keep our space activity sustainable. For the improvement in the ground safety related to the survived debris after the destructive re-entry of the rocket upper stages and the spacecrafts, the comprehensive considerations on the design and the disposal operation should be made. High-fidelity model-based re-entry safety analysis tool LS-DARC is under the development in JAXA. Purpose of this study is an establishment of quantitative assessment of the design and disposal operation change effect on the re-entry risk. Consequently, a) design for demise from the initial development phase, and b) accurate risk prediction by reducing epistemic uncertainty are realized. LS-DARC is multi-physics coupling analysis code including the aerodynamic and 6DoF trajectory analysis, surface heat flux distribution analysis, three-dimensional thermal transfer analysis. Establishment of the uncertainty quantification process of the LS-DARC models is essential in order to make it practical re-entry safety analysis tool. In this report, the uncertainty quantification process especially on the heat flux model is proposed and discussed. Research activities on the validation data acquisition by the high-enthalpy wind tunnel and the model validations are discussed., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2130003024, レポート番号: JAXA-SP-21-001

Published
2021

16. 展開型柔軟エアロシェル大気圏突入システムに関する研究

Author

YAMADA, Kazuhiko, SUZUKI, Kojiro, AKITA, Daisuke, ISHIMURA, Kosei, IMAMURA, Osamu, OTSU, Hirotaka, KAWAMURA, Masaaki, SHOJI, Yasuhiro, TAKAHASHI, Yusuke, TANNO, Hideyuki, TEZUKA, Asei, NAKAO, Tatsuro, NAKASHINO, Kyoichi, NAGATA, Yasunori, MIYAMOTO, Hideaki, HIROSE, Chikako, MORI, Koichi, MORIYOSHI, Takahiro, and WATANABE, Yasumasa

Abstract

令和3年度宇宙航行の力学シンポジウム（2021年12月20日-21日. オンライン開催), Symposium on Flight Mechanics and Astrodynamics: 2021 (December 20-21, 2021. Online Meeting), 著者人数: 19名, 資料番号: SA6000174019

Published
2021

17. 膨張波管HEK-X内の自由流温度、密度及び速度の評価

Author

HARA, Shigeru, SHIMAMURA, Kohei, and TANNO, Hideyuki

Abstract

令和3年度宇宙航行の力学シンポジウム（2021年12月20日-21日. オンライン開催), Symposium on Flight Mechanics and Astrodynamics: 2021 (December 20-21, 2021. Online Meeting), 資料番号: SA6000174030

Published
2021

21. Analysis of Second-Mode Amplitudes on Sharp Cones in Hypersonic Wind Tunnels

Author

Marineau, Eric C., Grossir, Guillaume, Wagner, Alexander, Leinemann, Madlen, Radespiel, Rolf, Chynoweth, Brandon C., Schneider, Steven P., Wagnild, Ross M., Casper, Katya M., and Tanno, Hideyuki

Subjects
Physics, 020301 aerospace & aeronautics, Hypersonic speed, Group (mathematics), Mode (statistics), Aerospace Engineering, Geometry, 02 engineering and technology, 01 natural sciences, 010305 fluids & plasmas, Amplitude, 0203 mechanical engineering, Cone (topology), Space and Planetary Science, 0103 physical sciences, Wind tunnel
Abstract

形態: カラー図版あり, Physical characteristics: Original contains color illustrations, Accepted: 2018-10-23, 資料番号: PA1910020000

Published
2019
Full Text
View/download PDF

22. High-Enthalpy Effects on Hypersonic Boundary-Layer Transition

Author

Wartemann, Viola, Wagner, Alexander, Wagnild, Ross, Pinna, Fabio, Miro, Miro Fernando, Johnson, Heath, and Tanno, Hideyuki

Subjects
LST, Hypersonic speed, Materials science, business.industry, Angle of attack, Enthalpy, Aerospace Engineering, High-Enthalpy Effects, Mechanics, Perfect gas, Computational fluid dynamics, High Enthalpy Shock Tunnel Göttingen, Stagnation point, Real-Gas Effects, Compressible flow, Boundary layer, Hypersonic Boundary-Layer Transition, Stability Analysis, Space and Planetary Science, business, PSE
Abstract

形態: カラー図版あり, Physical characteristics: Original contains color illustrations, Accepted: 2018-10-01, 資料番号: PA1910019000

Published
2019
Full Text
View/download PDF

23. Experimental Investigation of Roughness Effects on Transition on Blunt Spherical Capsule Shapes

Author

Radespiel, Rolf, Ali, Syed R. C., Munoz, Federico, Bowersox, Rodney, Leidy, Andrew, Kirk, Lindsay C., Reshotko, Eli, and Tanno, Hideyuki

Subjects
Adverse pressure gradient, Materials science, Space and Planetary Science, Angle of attack, Aerodynamic heating, digestive, oral, and skin physiology, Direct numerical simulation, Surface roughness, Stagnation enthalpy, Aerospace Engineering, Capsule, Mechanics, Surface finish
Abstract

形態: カラー図版あり, Physical characteristics: Original contains color illustrations, Accepted: 2018-10-22, 資料番号: PA1910021000

Published
2019
Full Text
View/download PDF

24. Measurement of Ultraviolet Radiative Heating Augmentation in HIEST Reflected Shock Tunnel

Author

Cruden, Brett A, Brandis, Aaron M, Olejniczak, Joseph, Grinstead, Jay, Kirk, Lindsay, Tanno, Hideyuki, and Komuro, Tomoyuki

Subjects
Fluid Mechanics And Thermodynamics
Abstract

Radiance measurements in air at enthalpies from 8-20 MJkg have been made over a 250mm diameter flat-faced test article in Japan Aerospace Exploration Agency's HIgh-Enthalpy Shock Tunnel (HIEST). Measurements were made in the ultraviolet region (200-400 nm wavelength) in an attempt to resolve the long-standing discrepancy between theoryand measurements of heat flux over a blunt body; this discrepancy is often attributed toradiation. The spectra obtained indicate the presence of atomic iron vapor in the flowfield.At the highest enthalpies, the radiance is at the blackbody limit. An attempt to model theradiance is made by taking a nominal CFD flowfield without any contamination productsand processing it through a line-by-line radiation simulation tool. Iron vapor is introducedinto the shocked gas ahead of the model and radiation computations are repeated; the molefraction of iron vapor is adjusted to match the data. For the higher enthalpy conditions, theradiance was strongly absorbed and it was necessary to adjust the temperature and NOdensity in the freestream to match the signal below 300 nm. Once the observed spectrawere satisfactorily matched, the radiance to the stagnation point was then computed. It isshown that the impurity radiation is sufficiently large to explain the discrepancy.

Published
2015

26. Boundary Layer Transition and Trip Effectiveness on an Apollo Capsule in the JAXA High Enthalpy Shock Tunnel (HIEST) Facility

Author

Kirk, Lindsay C, Lillard, Randolph P, Olejniczak, Joseph, and Tanno, Hideyuki

Subjects
Spacecraft Design, Testing And Performance, Fluid Mechanics And Thermodynamics
Abstract

Computational assessments were performed to size boundary layer trips for a scaled Apollo capsule model in the High Enthalpy Shock Tunnel (HIEST) facility at the JAXA Kakuda Space Center in Japan. For stagnation conditions between 2 MJ/kg and 20 MJ/kg and between 10 MPa and 60 MPa, the appropriate trips were determined to be between 0.2 mm and 1.3 mm high, which provided kappa/delta values on the heatshield from 0.15 to 2.25. The tripped configuration consisted of an insert with a series of diamond shaped trips along the heatshield downstream of the stagnation point. Surface heat flux measurements were obtained on a capsule with a 250 mm diameter, 6.4% scale model, and pressure measurements were taken at axial stations along the nozzle walls. At low enthalpy conditions, the computational predictions agree favorably to the test data along the heatshield centerline. However, agreement becomes less favorable as the enthalpy increases conditions. The measured surface heat flux on the heatshield from the HIEST facility was under-predicted by the computations in these cases. Both smooth and tripped configurations were tested for comparison, and a post-test computational analysis showed that kappa/delta values based on the as-measured stagnation conditions ranged between 0.5 and 1.2. Tripped configurations for both 0.6 mm and 0.8 mm trip heights were able to effectively trip the flow to fully turbulent for a range of freestream conditions.

Published
2015

27. FLDI(集光レーザー差動干渉計)による高温衝撃風洞HIESTにおける乱流遷移計測

Author

MANOHARAN, Rounak, SUZUKi, Shuntaro, KAWATA, Soma, SHIMAMURA, Kohei, TANNO, Hideyuki, ITO, Katsuhiro, YAMADA, Kazuhiko, and NAGATA, Yasunori

Abstract

令和2年度宇宙航行の力学シンポジウム（2020年12月14日-15日. オンライン開催), Symposium on Flight Mechanics and Astrodynamics: 2020 (December 14-15, 2020. Online Meeting), 資料番号: SA6000164018

Published
2020

28. 将来の惑星探査のための展開型柔軟シェルによる大気圏突入技術の研究

Author

YAMADA, Kazuhiko, SUZUKI, Kojiro, AKITA, Daisuke, ISHIMURA, Kosei, IMAMURA, Osamu, OTSU, Hirotaka, KAWAMURA, Masaaki, SHOJI, Yasuhiro, TAKAHASHI, Yusuke, TANNO, Hideyuki, TEZUKA, Asei, NAKAO, Tatsuo, NAKASHINO, Kyoichi, NAGATA, Yasunori, MIYAMOTO, Hideaki, MORI, Koichi, and WATANABE, Yasumasa

Abstract

令和2年度宇宙航行の力学シンポジウム（2020年12月14日-15日. オンライン開催), Symposium on Flight Mechanics and Astrodynamics: 2020 (December 14-15, 2020. Online Meeting), 著者人数: 17名, 資料番号: SA6000164019

Published
2020

29. Temperature measurement at inner wall of expansion tube

Author

FUKUMARU, Sho, FUJIWARA, Yusuke, OKAMOTO, Takashi, SHIMAMURA, Kohei, YAMADA, Kazuhiko, TANNO, Hideyuki, and KOMURO, Tomoyuki

Subjects
Shock Wave, Expansion Tube, Coaxial Thermocouple
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148110, レポート番号: 3C2-1[若]

Published
2020

30. LES of Rotating Detonation with a Non-premixed CH4/O2 Injection

Author

MATSUYAMA, Shingo, IWATA, Kazuya, KOJIMA, Makoto, NUNOME, Yoshio, TANNO, Hideyuki, KAWASHIMA, Hideto, and MIZUKAKI, Toshiharu

Subjects
Rocket engine combustor, Methane-oxygen combustion, Large-Eddy simulation, Detonation
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148030, レポート番号: 1C1-2

Published
2020

31. Status of wave front visualization development by interferometer for elucidation of detailed structure of rotating detonation wave

Author

IWASAKI, Fumihiko, MORI, Misato, SHIMIZU, Ryunosuke, MIZUKAKI, Toshiharu, KOJIMA, Atsushi, IWATA, Kazuya, NUNOME, Yoshio, TANNO, Hideyuki, and KAWASHIMA, Hideto

Subjects
Point Diffraction Interferometer, Detonation, Rotating Detonation Engine, Visualization
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148029, レポート番号: 1C1-1

Published
2020

32. Visualization measurement of density of hypersonic flow field using shearing interferometer

Author

UCHIBE, Ginji, SHIMAMURA, Kohei, TAKAHASHI, Yusuke, YAMADA Kazuhiko, TANNO, Hideyuki, and KOMURO, Tomoyuki

Subjects
Shearing interferometer, Hypersonic flow, HAYABUSA, HIEST
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148107, レポート番号: 3C1-4[若]

Published
2020

33. Experimental Investigation on the Relationship Between Thrust Performance and Detonation Propagation Mode of Methane/Oxygen Rotating Detonation Rocket Engine

Author

IWATA, Kazuya, KOJIMA, Makoto, NUNOME, Yoshio, KAWASHIMA, Hideto, TANNO, Hideyuki, and MATSUYAMA, Shingo

Subjects
specific thrust, methane, Rotating Detonation Engine, chemiluminescence
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148033, レポート番号: 1C2-1

Published
2020

34. Radiation measurement of shock layer with model embedded optical fibers

Author

BRETT, A. Cruden, JOSEPH, Olejniczak, ADAM, Amar, and TANNO, Hideyuki

Subjects
Aero heating, Shock tunnel, Radiation, Hypersonics
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148106, レポート番号: 3C1-3

Published
2020

35. Aerodynamic force measurement of blunt cones in high-enthalpy shock tunnel HIEST

Author

NOGUCHI, Shunsuke, TANNO, Hideyuki, and ITOH, Katsuhiro

Subjects
Aerodynamics, Shock tunnel, High-temperature real-gas effect, Hypersonic
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148121, レポート番号: P-07[若]

Published
2020

36. Core Flow Estimation and Heat Flux Measurement around Hayabusa type SRC model in the expansion tube

Author

FUJIWARA, Yusuke, FUKUMARU, Sho, SHIMAMURA, Kohei, YAMADA, Kazuhiko, TANNO, Hideyuki, KOMURO, Tomoyuki, and TEZUKA, Asei

Subjects
Re-entry, Sample Return Capsule, Heat Flux, Expansion Tube
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148108, レポート番号: 3C1-5[若]

Published
2020

37. Laser Absorption Diagnostics with Multipass of HEK-X

Author

KOBAYASHI, Ryuji, OKAMOTO, Takashi, MATSUI, Makoto, TANNO, Hideyuki, and YAMADA, Kazuhiko

Subjects
HEK-X, Herriott Multipass Cell, Expansion Tube, Laser Absorption Spectroscopy
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148109, レポート番号: 3C1-6[若]

Published
2020

38. Numerical Analysis for Non-linear Growth in Hypersonic Boundary Layer

Author

UDA, Yuichiro, SATO, Shintaro, OHNISHI, Naofumi, and TANNO, Hideyuki

Subjects
Flow Instability, CFD, Hypersonic
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148093, レポート番号: 3B1-4[若]

Published
2020

39. Modeling of Shock Wave Propagation and Attenuation in a Shock Tube

Author

MURATA, Kensuke, SAKAI, Takeharu, and TANNO, Hideyuki

Subjects
Shock Wave, Boundary Layer, Attenuation, Moving grid
Abstract

2019年度衝撃波シンポジウム (2020年3月4日-6日. 神戸大学 海事科学研究科（深江キャンパス)）神戸市, 兵庫県, Symposium on Shock Waves in Japan, FY2019 (March 3-4, 2020. Kobe University), Kobe, Hyogo Japan, 2019年度衝撃波シンポジウムは、新型コロナウイルスの感染拡大防止のため開催中止, 資料番号: SA6000148113, レポート番号: 3C2-4[若]

Published
2020

45. 高温衝撃風洞を用いたはやぶさカプセル周りの定量的可視化計測

Author

UCHIBE, Ginji, SHIMAMURA, Kohei, TAKAHASHI, Yusuke, YAMADA, Kazuhiko, TANNO, Hideyuki, and KOMURO, Tomoyuki

Abstract

令和元年度宇宙航行の力学シンポジウム（2019年12月9日-10日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県, Symposium on Flight Mechanics and Astrodynamics: 2019 (December 9-10, 2019. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan, 資料番号: SA6000154031

Published
2019

47. Technical issues of aero heating test in shock tunnel HIEST

Author

Tanno, Hideyuki

Subjects
Shock tunnel, Boundary layer transition, Hypersonic
Abstract

平成30年度衝撃波シンポジウム (2019年3月5日-7日. 横浜国立大学経済・経営学部講義棟1号館 ）横浜市, 神奈川県, Symposium on Shock Waves in Japan, FY2018 (March 5-7, 2019. Yokohama National University), Yokohama, Kanagawa, 資料番号: SA6000134056, レポート番号: 2A2-2

Published
2019

48. Experiment for Understanding Re-entry Environment of Sample Return Capsule in Expansion Tube

Author

Fujiwara, Yusuke, Uchibe, Ginji, Shimamura, Kohei, Yamada, Kazuhiko, Tanno, Hideyuki, Komuro, Tomoyuki, and Tezuka, Asei

Subjects
Re-entry, Heat Flux, Expansion Tube
Abstract

平成30年度衝撃波シンポジウム (2019年3月5日-7日. 横浜国立大学経済・経営学部講義棟1号館 ）横浜市, 神奈川県, Symposium on Shock Waves in Japan, FY2018 (March 5-7, 2019. Yokohama National University), Yokohama, Kanagawa, 資料番号: SA6000134050, レポート番号: 2A1-1 [若]

Published
2019

49. Aerodynamic Force Measurement Technique by Free-flight Test for Scramjet Powered Vehicle in Shock Tunnel

Author

Tanno, Marie, Nagai, Hiroki, Tanno, Hideyuki, and Komuro, Tomoyuki

Subjects
Shock tunnel, Scramjet, Free-flight, Hypersonic
Abstract

平成30年度衝撃波シンポジウム (2019年3月5日-7日. 横浜国立大学経済・経営学部講義棟1号館 ）横浜市, 神奈川県, Symposium on Shock Waves in Japan, FY2018 (March 5-7, 2019. Yokohama National University), Yokohama, Kanagawa, 資料番号: SA6000134036, レポート番号: 1C1-3 [若]

Published
2019

50. Template Paper for the Symposium on Shock Waves, 2018 JAPAN

Author

Matsui, Makoto, Okamoto, Tatakashi, Ikutomo, Ayaka, Kobayashi, Ryuji, Yamada, Kazuhiko, and Tanno, Hideyuki

Subjects
Expansion tube, flow diagnostics, laser absorption spectroscopy
Abstract

平成30年度衝撃波シンポジウム (2019年3月5日-7日. 横浜国立大学経済・経営学部講義棟1号館 ）横浜市, 神奈川県, Symposium on Shock Waves in Japan, FY2018 (March 5-7, 2019. Yokohama National University), Yokohama, Kanagawa, 資料番号: SA6000134083, レポート番号: 3A1-2

Published
2019

Catalog

Books, media, physical & digital resources
See catalog results