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Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms [microform] / Nathan S. Jacobson (NASA/TM ; 1999-208907)

Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms [microform] / Nathan S. Jacobson (NASA/TM ; 1999-208907)
マイクロ図書
1999<YCA-NAS 1.15:208907>
国立国会図書館
  • 件名Graphite Furnaces Hypersonic wind tunnels

Langley 8-ft. HTT test 139 gas analyses [microform] / Danny R. Sprinkle and Patricia P. Davis (NASA/TM ; 1999-209712)

Langley 8-ft. HTT test 139 gas analyses [microform] / Danny R. Sprinkle and Patricia P. Davis (NASA/TM ; 1999-209712)
マイクロ図書
1999<YCA-NAS 1.15:209712>
国立国会図書館
  • 件名...s spectroscopy Hypersonic wind tunnels Blowdown wind tunnels

Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF [microform] / H. Douglas Perkins, Scott R. Thomas, and William D. Pack (NASA technical memorandum ; 107384)

Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF [microform] / H. Douglas Perkins, Scott R. Thomas, and William D. Pack (NASA technical memorandum ; 107384)
マイクロ図書
1996<YCA-NAS 1.15:107384>
国立国会図書館
  • 件名Integral rocket ramjets Engine tests Hypersonic speed Hypersonic wind tunnels

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation [microform] / Lawrence D. Huebner, Marc W. Kniskern, William J. Monta (NASA technical memorandum ; 4441)

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation [microform] / Lawrence D. Huebner, Marc W. Kniskern, William J. Monta (NASA technical memorandum ; 4441)
マイクロ図書
1993<YCA-NAS 1.15:4441>
国立国会図書館
  • 件名Hypersonic wind tunnels Aerodynamics, Hypersonic

Nonintrusive fast response oxygen monitoring system for high temperature flows [microform] / Daniel B. Oh and Alan C. Stanton (NASA contractor report ; 4553)

Nonintrusive fast response oxygen monitoring system for high temperature flows [microform] / Daniel B. Oh and Alan C. Stanton (NASA contractor report ; 4553)
マイクロ図書
1993<YCA-NAS 1.26:4553>
国立国会図書館
  • 件名Hypersonic wind tunnels Modulation spectroscopy

Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels microform / Gregory M. Buck (NASA TM ; 112159)

Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels microform / Gregory M. Buck (NASA TM ; 112159)
マイクロ図書
1995<YCA-NAS 1.15:112159>
国立国会図書館
  • 件名Hypersonic wind tunnels Surface temperature Pressure...

Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21) [microform] / A.M. Springer ([NASA technical paper] ; NASA/TP-1998-208396)

Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21) [microform] / A.M. Springer ([NASA technical paper] ; NASA/TP-1998-208396)
マイクロ図書
1998<YCA-NAS 1.60:208396>
国立国会図書館
  • 件名Hypersonic wind tunnels Wind tunnel tests Supersonic...

Enhancing U.S. competitiveness : NASA hypersonics research and wind tunnel programs : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, second session, March 15, 1994

Enhancing U.S. competitiveness : NASA hypersonics research and wind tunnel programs : hearing before the Subcommittee on Technology, Environment, and Aviation of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, second session, March 15, 1994
マイクロ図書
1994<YCA-Y 4.SCI 2:103/98>
国立国会図書館
  • 件名...d expenditures Hypersonic wind tunnels Aerodynamics, Hypersonic -- ...

標準模型6分力試験結果を用いたJAXA1.27m極超音速風洞におけるデータバラつきに関する再評価

標準模型6分力試験結果を用いたJAXA1.27m極超音速風洞におけるデータバラつきに関する再評価
デジタル文書・図像類
藤井, 啓介, 津田, 尚一, 小山, 忠勇, 高間, 良樹, 中川, 宗敬, 板橋, 幸広, 中村, 晃祥, Fujii, Keisuke, Tsuda, Shoichi, Koyama, Tadao, Takama, Yoshiki, Nakagawa, Muneyoshi, Itabashi, Yukihiro, Nakamura, Akiyoshi宇宙航空研究開発機構(JAXA)2016-11-07宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-16-004p.1-15
全国の図書館
  • 件名Hypersonic wind tunnel deviation in Mach number aero...
  • 一般注記... in JAXA 1.27m hypersonic wind tunnel suggests that the perfect gas...
  • 並列タイトル等（連結）Deviation in Standard Model Force Measurements in JAXA 1.27m Hypersonic Wind Tunnel

Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly [microform] / Gregory J. Brauckmann; John W. Paulson, Jr.; K. James Weilmuenster (NASA-TM ; 112155)

Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly [microform] / Gregory J. Brauckmann; John W. Paulson, Jr.; K. James Weilmuenster (NASA-TM ; 112155)
マイクロ図書
1995<YCA-NAS 1.15:112155>
国立国会図書館
  • 件名...d tunnel tests Hypersonic wind tunnels Pitching moments Temperature...

Aeronautical facilities catalogue / compiled and edited by Frank E. Peñaranda and M. Shannon Freda (NASA RP ; 1132)

Aeronautical facilities catalogue / compiled and edited by Frank E. Peñaranda and M. Shannon Freda (NASA RP ; 1132)
マイクロ図書
1985<YCA-NAS 1.61:1132/v.1>
国立国会図書館
  • 件名Hypersonic wind tunnels -- Catalogs Supersonic wind ...

1.27m極超音速風洞における水分管理

1.27m極超音速風洞における水分管理
デジタル文書・図像類
永井, 伸治, 津田, 尚一, 小山, 忠勇, 平林, 則明, 関根, 英夫, Nagai, Shinji, Tsuda, Shoichi, Koyama, Tadao, Hirabayashi, Noriaki, Sekine, Hideo航空宇宙技術研究所2001-12航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1436
全国の図書館
  • 件名極超音速風洞 校正 湿度 燃焼 ピトー管 圧力分布 加熱 hypersonic wind tunnel calibration humidity combusti...
  • 一般注記...oratory 1.27 m hypersonic wind tunnel immediately after a humid com...
  • 並列タイトル等（連結）Humidity management for the NAL 1.27 m hypersonic wind tunnel

Comparative force/heat flux measurements between JAXA hypersonic test facilities using standard model HB-2

Comparative force/heat flux measurements between JAXA hypersonic test facilities using standard model HB-2
デジタル文書・図像類
口石, 茂, 渡辺, 重哉, 植田, 修一, 丹野, 英幸, 小室, 智幸, 佐藤, 和雄, 伊藤, 勝宏, Kuchiishi, Shigeru, Watanabe, Shigeya, Ueda, Shuichi, Tanno, Hideyuki, Komuro, Tomoyuki, Sato, Kazuo, Ito, Katsuhiro宇宙航空研究開発機構2006-03-31宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-05-030E
全国の図書館
  • 件名...ynamic heating hypersonic wind tunnel
  • 一般注記...blow-down type hypersonic wind tunnel and to allevia......blow-down type hypersonic wind tunnel showed good agreement in the ...

Effect of airframe configuration on condition of airflow to engine in hypersonic flow

Effect of airframe configuration on condition of airflow to engine in hypersonic flow
デジタル文書・図像類
苅田, 丈士, 加藤, 周徳, 小寺, 正敏, 工藤, 賢司, 村上, 淳郎, 泉川, 宗男, 渡辺, 修一, Kanda, Takeshi, Kato, Kanenori, Kodera, Masatoshi, Kudo, Kenji, Murakami, Atsuo, Izumikawa, Muneo, Watanabe, Shuichi宇宙航空研究開発機構2007-12-28宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-07-007E
全国の図書館
  • 件名...nd tunnel test hypersonic wind tunnel wind tunnel model Mach number...

Advances in hypervelocity techniques; proceedings. Edited by Arthur M. Krill. Sponsored by University of Denver, Denver Research Institute, 20 and 21 March 1962.

Advances in hypervelocity techniques; proceedings. Edited by Arthur M. Krill. Sponsored by University of Denver, Denver Research Institute, 20 and 21 March 1962.
紙図書
Distributed by Plenum Press[1962]<629.1323-S989a>
国立国会図書館
  • 件名Hypersonic wind tunnels -- Congresses. Aerodynamics,...

Comparative force/heat flux measurements between JAXA hypersonic test facilities using standard model HB-2

Comparative force/heat flux measurements between JAXA hypersonic test facilities using standard model HB-2
デジタル文書・図像類
口石, 茂, 渡辺, 重哉, 永井, 伸治, 津田, 尚一, 小山, 忠勇, 平林, 則明, 関根, 英夫, 穂積, 弘一, Kuchiishi, Shigeru, Watanabe, Shigeya, Nagai, Shinji, Tsuda, Shoichi, Koyama, Tadao, Hirabayashi, Noriaki, Sekine, Hideo, Hozumi, Koichi宇宙航空研究開発機構2005-03-31宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-04-035E
全国の図書館
  • 件名...力試験 弾道学 非侵襲的測定 hypersonic wind tunnel performance test heat flux ae...
  • 一般注記... in the 1.27 m Hypersonic Wind Tunnel (HWT) of the Japan Aerospace ...
  • 並列タイトル等（連結）1.27m極超音速風洞測定結果 HB-2形状標準模型を用いたJAXA極超音速風洞間力／加熱率対応風試 1.27 m hypersonic wind tunnel results

極超音速流中斜円柱付着線上境界層遷移への鈍頭度の効果に関する実験

極超音速流中斜円柱付着線上境界層遷移への鈍頭度の効果に関する実験
デジタル文書・図像類
藤井, 啓介, 小山, 忠勇, 津田, 尚一, 平林, 則明, 関根, 英夫, 永井, 伸治, 榊原, 盛三, 穂積, 弘一, Fujii, Keisuke, Koyama, Tadao, Tsuda, Shoichi, Hirabayashi, Noriaki, Sekine, Hideo, Nagai, Shinji, Sakakibara, Seizo, Hozumi, Koichi航空宇宙技術研究所2000-10航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory753p.1-17
全国の図書館
  • 件名...ypersonic flow hypersonic wind tunnel test compressible flow
  • 一般注記...conducted in a hypersonic wind tunnel. The tests wer......those of other hypersonic wind tunnel tests. Tests for the hemisphe...

1.27m、マッハ10極超音速風洞の気流検定結果について

1.27m、マッハ10極超音速風洞の気流検定結果について
デジタル文書・図像類
平林, 則明, 小山, 忠勇, 津田, 尚一, 関根, 英夫, 永井, 伸治, 榊原, 盛三, Hirabayashi, Noriaki, Koyama, Tadao, Tsuda, Shoichi, Sekine, Hideo, Nagai, Shinji, Sakakibara, Seizo航空宇宙技術研究所2000-07航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory45p.113-120
全国の図書館
  • 件名...吸込筒 一様性 計算流体力学 hypersonic wind tunnel air flow nozzle smoothing met...
  • 一般注記...ある。 The 1.27 m hypersonic wind tunnel was constructed at National A...

極超音速風洞データ処理装置の更新について

極超音速風洞データ処理装置の更新について
デジタル文書・図像類
津田, 尚一, 小山, 忠勇, Tsuda, Shoichi, Koyama, Tadao航空宇宙技術研究所1999-03航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory737p.1-32
全国の図書館
  • 件名...理ソフトウェア 計測システム hypersonic wind tunnel facility replacement data pro...
  • 一般注記...の更新の概要について述べる。 Hypersonic wind tunnel experiments, s......ce Laboratory) hypersonic wind tunnel system consist......em for the NAL hypersonic wind tunnel system including the data acq...
  • 並列タイトル等（連結）Replacement of the data processing system for the NAL Hypersonic Wind Tunnel System

大型極超音速風洞用高温高圧配管の熱設計

大型極超音速風洞用高温高圧配管の熱設計
デジタル文書・図像類
永井, 伸治, 津田, 尚一, 平林, 則明, 関根, 英夫, 榊原, 盛三, 下平, 一雄, 入野, 光博, Nagai, Shinji, Tsuda, Shoichi, Hirabayashi, Noriaki, Sekine, Hideo, Sakakibara, Seizo, Shimodaira, Kazuo, Irino, Mitsuhiro航空宇宙技術研究所1998-06航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory733p.1-19
全国の図書館
  • 件名...巻き 2重円筒構造 強制水冷 hypersonic wind tunnel hot duct thermal insulation s...
  • 一般注記...e of the large hypersonic wind tunnel with two newly designed therm...
  • 並列タイトル等（連結）Thermal design of 10 m-long hot duct for large hypersonic wind tunnel
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