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System identification of a vortex lattice aerodynamic model [microform] / Jer-Nan Juang, Denis Kholodar, Earl H. Dowell ([NASA technical memorandum] ; NASA/TM-2001-211229)

System identification of a vortex lattice aerodynamic model [microform] / Jer-Nan Juang, Denis Kholodar, Earl H. Dowell ([NASA technical memorandum] ; NASA/TM-2001-211229)
Microform図書
2001<YCA-NAS 1.15:211229>
National Diet Library
  • Subject Heading...haracteristics Delta wings Vortex lattice method Unstea...

Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations [microform] / Robert M. Bennett and Charlotte E. Walker ([NASA technical memorandum] ; NASA/TM-1999-209104)

Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations [microform] / Robert M. Bennett and Charlotte E. Walker ([NASA technical memorandum] ; NASA/TM-1999-209104)
Microform図書
1999<YCA-NAS 1.15:209104>
National Diet Library
  • Subject HeadingComputational fluid dynamics Delta wings Airfoil profiles Control sur...

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65⁰ delta wings varying in leading-edge radius and camber [microform] / S. Naomi McMillin ... [et al.] (NASA technical memorandum ; 4673)

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65⁰ delta wings varying in leading-edge radius and camber [microform] / S. Naomi McMillin ... [et al.] (NASA technical memorandum ; 4673)
Microform図書
1996<YCA-NAS 1.15:4673>
National Diet Library
  • Subject HeadingDelta wings Flow visualization Leading e...
  • Alternative Title... for three 65⁰ delta wings varying in leading edge radi...
  • Alternative Title... for three 65⁰ delta wings varying in leading edge radi...

Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications [microform] : final report for the period December 1, 1995 through Novemeber 30, 1996 / principal investigator, Osama A. Kandil ; submitted by the Old Dominion University Research Foundation ([NASA contractor report] ; NASA-CR-203244)

Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications [microform] : final report for the period December 1, 1995 through Novemeber 30, 1996 / principal investigator, Osama A. Kandil ; submitted by the Old Dominion University Research Foundation ([NASA contractor report] ; NASA-CR-203244)
Microform図書
1997<YCA-NAS 1.26:203244>
National Diet Library
  • Subject HeadingComputational fluid dynamics Delta wings Aeroelasticity Wing tips Vor...

An overview of an experimental demonstration aerotow program [microform] / James E. Murray ... [et al.] (NASA/TM ; 1998-206566)

An overview of an experimental demonstration aerotow program [microform] / James E. Murray ... [et al.] (NASA/TM ; 1998-206566)
Microform図書
1998<YCA-NAS 1.15:206566>
National Diet Library
  • Subject HeadingTetherlines Towing Tethering Delta wings Flight tests Launch vehicles...

Effective control of computationally simulated wing rock in subsonic flow [microform] / Osama A. Kandil and Margaret A. Menzies

Effective control of computationally simulated wing rock in subsonic flow [microform] / Osama A. Kandil and Margaret A. Menzies
Microform図書
1997<YCA-NAS 1.26:203247>
National Diet Library
  • Subject HeadingNavier-Stokes equation Delta wings Rigid structures Difference ...

Experimental surface pressure data obtained on 65⁰ delta wing across Reynolds number and Mach number ranges [microform] / Julio Chu and James M. Luckring (NASA technical memorandum ; 4645)

Experimental surface pressure data obtained on 65⁰ delta wing across Reynolds number and Mach number ranges [microform] / Julio Chu and James M. Luckring (NASA technical memorandum ; 4645)
Microform図書
1996<YCA-NAS 1.15:4645>
National Diet Library
  • Subject HeadingWind tunnel tests Delta wings Leading edges Reynolds numbe...

Natural rolling responses of a delta wing in transonic and subsonic flows [microform] / Margaret A. Menzies and O. Kandil ([NASA contractor report] ; NASA-CR-203246)

Natural rolling responses of a delta wing in transonic and subsonic flows [microform] / Margaret A. Menzies and O. Kandil ([NASA contractor report] ; NASA-CR-203246)
Microform図書
1996<YCA-NAS 1.26:203246>
National Diet Library
  • Subject Heading...on Swept wings Delta wings Rigid structures Slender win...

Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : a multidisciplinary problem / by Margaret Anne Menzies ; a dissertation submitted to the Faculty of Old Dominion University in partial fulfillment of the requirement for the degree of Doctor of Philosphy, Aerospace Engineering, Old Dominion University ([NASA contractor report] ; NASA-CR-203248)

Unsteady, transonic flow around delta wings undergoing coupled and natural modes response : a multidisciplinary problem / by Margaret Anne Menzies ; a dissertation submitted to the Faculty of Old Dominion University in partial fulfillment of the requirement for the degree of Doctor of Philosphy, Aerospace Engineering, Old Dominion University ([NASA contractor report] ; NASA-CR-203248)
Microform図書
1996<YCA-NAS 1.26:203248>
National Diet Library
  • Subject HeadingTransonic flow Unsteady flow Delta wings Aerodynamic coefficients Nav...

Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle [microform] / Roger A. Lepsch, Jr. and George M. Ware, Ian O. MacConochie (NASA technical memorandum ; 4726)

Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle [microform] / Roger A. Lepsch, Jr. and George M. Ware, Ian O. MacConochie (NASA technical memorandum ; 4726)
Microform図書
1996<YCA-NAS 1.15:4726>
National Diet Library
  • Subject HeadingWind tunnel tests Delta wings Angle of attack Rolling mome...

超音速デルタ翼の振動特性と安定限界の推定 第1報 定常な不規則応答のオンライン時系列解析

超音速デルタ翼の振動特性と安定限界の推定 第1報 定常な不規則応答のオンライン時系列解析
Digital文書・図像類
安藤, 泰勝, 松崎, 雄嗣, 峯岸, 正勝, 江尻, 宏, 榊原, 盛三, 野田, 順一, 石田, 清道, ANDO, Yasukatsu, MATSUZAKI, Yuji, MINEGISHI, Masakatsu, EJIRI, Hiroshi, SAKAKIBARA, Seizo, NODA, Junichi, ISHIDA, Kiyomichi航空宇宙技術研究所1992-04航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-11531153p.17-
Other Libraries in Japan
  • Subject HeadingSupersonic delta wing; vibration-mode parameter; ...
  • Note (General)... on supersonic delta wing models to enable system evalu...
  • Alternative Title... on Supersonic Delta Wings Part 1 On-Line Time Series A...

Experimental Studies of Vortex Flaps and Vortex Plates Part 1. 0.53m Span 60deg Delta Wing

Experimental Studies of Vortex Flaps and Vortex Plates Part 1. 0.53m Span 60deg Delta Wing
Digital文書・図像類
李家, 賢一, RINOIE, Kenichi航空宇宙技術研究所1992-03Technical Report of National Aerospace Laboratory TR-1140T1140Tp.16-
Other Libraries in Japan
  • Subject Headinglow-speed aerodynamics; delta wing; vortex flap; votex plate; ...
  • Note (General)...on a 60 degree delta wing model. Results......on between the delta wing and the vortex plate. 資料番号: N...

ボルテックス･フラップ付きデルタ翼の低速空力特性について:後退角60度と70度の比較

ボルテックス･フラップ付きデルタ翼の低速空力特性について:後退角60度と70度の比較
Digital文書・図像類
李家, 賢一, 藤田, 敏美, 岩崎, 昭人, 藤枝, 郭俊, Rinoie, Kenichi, Fujita, Toshimi, Iwasaki, Akihito, Fujieda, Hirotoshi航空宇宙技術研究所1994-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1245p.1-13
Other Libraries in Japan
  • Subject Heading...力学 vortex flap delta wing aerodynamics low speed delta wing characteristic...... visualization delta wing lift to drag ratio sweepback ...
  • Note (General)...de on a 70 deg delta wing model with tap...... m span 70 deg delta wing model. The res......deg and 70 deg delta wing models. Flow p......tion of 70 deg delta wing were found to ......hose of 60 deg delta wing. The maximum l......ent for 70 deg delta wing is attained when a separated ...
  • Alternative Title...acteristics of delta wings with vortex f......deg and 70 deg Delta wings

閉塞修正方法の検討:デルタ翼模型の低速風洞試験の実施と閉塞修正係数式の変形

閉塞修正方法の検討:デルタ翼模型の低速風洞試験の実施と閉塞修正係数式の変形
Digital文書・図像類
奥山, 政広, 岩崎, 昭人, 藤田, 敏美, Okuyama, Masahiro, Iwasaki, Akihito, Fujita, Toshimi航空宇宙技術研究所1997-01航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory707p.1-13
Other Libraries in Japan
  • Subject Heading...rection method delta wing low speed wind tunnel blockag...
  • Note (General)...ically similar delta wings with different reference are...
  • Alternative TitleThe blockage correction methods for low-speed wind tunnel testing on delta wings

飛行試験データによるALFLEX実験機の空力特性推定と風洞試験データとの比較評価

飛行試験データによるALFLEX実験機の空力特性推定と風洞試験データとの比較評価
Digital文書・図像類
柳原, 正明, 重見, 仁, 水藤, 貴靖, Yanagihara, Masaaki, Shigemi, Masashi, Suito, Takanobu航空宇宙技術研究所1998-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1353p.1-29
Other Libraries in Japan
  • Subject Heading...nd tunnel test delta wing tip fin hanging flight test H...
  • Note (General)...vehicle with a delta wing and tip fins. The tests for t...

デルタ翼のウイングロックと相平面法による解析

デルタ翼のウイングロックと相平面法による解析
Digital文書・図像類
楯, 篤志, 野田, 順一, 吉永, 崇, Tate, Atsushi, Noda, Junichi, Yoshinaga, Takashi航空宇宙技術研究所1995-04航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1266p.1-18
Other Libraries in Japan
  • Subject Heading...mics wing rock delta wing phase plane method high angle...
  • Note (General)...motion of thin delta wings with varying ......regions of the delta wings were obtained...... roll axis vs. delta wing sweep angle. An analytical ex...
  • Alternative TitleWing rock of delta wings with an analysis by the phas...

超音速フラッタ停止装置の開発

超音速フラッタ停止装置の開発
Digital文書・図像類
峯岸, 正勝, 安藤, 泰勝, 松崎, 雄嗣, 江尻, 宏, 野田, 順一, 関根, 英夫, 楯, 篤志, 渡辺, 光則, Minegishi, Masakatsu, Ando, Yasukatsu, Matsuzaki, Yuji, Ejiri, Hiroshi, Noda, Junichi, Sekine, Hideo, Tate, Atsushi, Watanabe, Mitsunori航空宇宙技術研究所1996-05航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory693p.1-8
Other Libraries in Japan
  • Subject Heading...洞試験 supersonic delta wing flutter test flutter emergenc...
  • Note (General)... of supersonic delta wings and is found to yield good r...

流れの可視化用小型回流水槽

流れの可視化用小型回流水槽
Digital文書・図像類
進藤, 重美, 柳, 良二, 三村, 富嗣雄, 坂田, 公夫, Shindo, Shigemi, Yanagi, Ryoji, Mimura, Fujio, Sakata, Kimio航空宇宙技術研究所1995-08航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory686p.1-38
Other Libraries in Japan
  • Subject Heading...yer separation delta wing water channel for observation...
  • Note (General)... flow around a delta wing and flow properties of a tele...

極超音速飛行実験機の衝撃風洞試験

極超音速飛行実験機の衝撃風洞試験
Digital文書・図像類
白水, 正男, 渡辺, 重哉, 山崎, 喬, 伊藤, 健, 和田, 安弘, 永井, 伸治, 村上, 哲, 溝端, 一秀, 少路, 宏和, Shirouzu, Masao, Watanabe, Shigeya, Yamazaki, Takashi, Ito, Takeshi, Wada, Yasuhiro, Nagai, Shinji, Murakami, Akira, Mizobata, Kazuhide, Shoji, Hirokazu航空宇宙技術研究所1997-01航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory708p.1-16
Other Libraries in Japan
  • Subject Heading...ane J 1 rocket delta wing winged configuration lifting ...
  • Note (General)...One model used delta wings (HRV02) and the other had th...

超音速デルタ翼の振動特性と安定限界の推定　第2報:非定常な不規則応答の局所定常時系列解析

超音速デルタ翼の振動特性と安定限界の推定　第2報:非定常な不規則応答の局所定常時系列解析
Digital文書・図像類
峯岸, 正勝, 安藤, 泰勝, 松崎, 雄嗣, 江尻, 宏, 榊原, 盛三, 野田, 順一, 石田, 清道, 関根, 英夫, 楯, 篤志, 渡辺, 光則, Minegishi, Masakatu, Ando, Yasukatu, Matsuzaki, Yuji, Ejiri, Hiroshi, Sakakibara, Seizo, Noda, Jyunichi, Ishida, Kiyomichi, Sekine, Hideo, Tate, Atsushi, Watanabe, Mitsunori航空宇宙技術研究所1992-09航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1179p.1-19
Other Libraries in Japan
  • Subject Heading...upersonic flow delta wing aerodynamics vibration charac...
  • Note (General)...m responses in delta wings under superso......ted cantilever delta wings failed during supersonic blo...
  • Alternative Title... on supersonic delta wings. Part 2: Locally-stationary ...
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