yr 〜
yr

Search results 21

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 Unstead...

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 surf...

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 ed...
  • Alternative Title... for three 65⁰ delta wings varying in leading edge radiu...
  • Alternative Title... for three 65⁰ delta wings varying in leading edge radiu...

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 Vort...

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 e...

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 number...

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 wing...

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 Navi...

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 momen...

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
  • Alternative Title... on Supersonic Delta Wings Part 1 On-Line Time Series An...
  • Alternative Title... on Supersonic Delta Wings Part 1 On-Line Time Series An...

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

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
  • Alternative Title...acteristics of delta wings with vortex fl......deg and 70 deg Delta wings
  • Alternative Title...acteristics of delta wings with vortex fl......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
  • Note (General)...ically similar delta wings with different reference area...
  • Alternative TitleThe blockage correction methods for low-speed wind tunnel testing on delta wings
  • 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

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
  • Note (General)...motion of thin delta wings with varying s......regions of the delta wings were obtained and compared wi...
  • Alternative TitleWing rock of delta wings with an analysis by the phase...
  • Alternative TitleWing rock of delta wings with an analysis by the phase...

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
  • Note (General)... of supersonic delta wings and is found to yield good re...

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

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
  • Note (General)...One model used delta wings (HRV02) and the other had the...

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
  • Note (General)...m responses in delta wings under superson......ted cantilever delta wings failed during supersonic blow...
  • Alternative Title... on supersonic delta wings. Part 2: Locally-stationary t...
  • Alternative Title... on supersonic delta wings. Part 2: Locally-stationary t...