年 〜
年

検索結果 5 件

Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter (NASA/TP ; 1999-209093)

Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle [microform] / Scott C. Asbury and Craig A. Hunter (NASA/TP ; 1999-209093)
マイクロ図書
1999<YCA-NAS 1.60:209093>
国立国会図書館
  • 件名...ts Nozzle flow Oblique shock waves Flow visualization

Screech tones from rectangular jets with spanwise oblique shock-cell structures [microform] : [final contractor report] / Ganesh Raman (NASA contractor report ; 198417)

Screech tones from rectangular jets with spanwise oblique shock-cell structures [microform] : [final contractor report] / Ganesh Raman (NASA contractor report ; 198417)
マイクロ図書
1996<YCA-NAS 1.26:198417>
国立国会図書館
  • 件名Oblique shock waves Acoustic fatigue Aircraft de...

Computation of thermally perfect properties of oblique shock waves [microform] : under contract NAS1-19000 / Kenneth E. Tatum (NASA contractor report ; 4749)

Computation of thermally perfect properties of oblique shock waves [microform] : under contract NAS1-19000 / Kenneth E. Tatum (NASA contractor report ; 4749)
マイクロ図書
1996<YCA-NAS 1.26:4749>
国立国会図書館
  • 件名Oblique shock waves Computational fluid dynamics...

Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction [microform] / D.O. Davis, B.P. Willis, and W.R. Hingst (NASA/TM ; 1998-206974)

Flowfield measurements in a slot-bled oblique shock wave and turbulent boundary-layer interaction [microform] / D.O. Davis, B.P. Willis, and W.R. Hingst (NASA/TM ; 1998-206974)
マイクロ図書
1998<YCA-NAS 1.15:206974>
国立国会図書館
  • 件名Flow measurement Oblique shock waves Boundary layer control Bound...
  • 並列タイトル等（連結）Flowfield measurements in a slot bled oblique shock wave and turbulent boundary-layer ...
  • 並列タイトル等Flowfield measurements in a slot bled oblique shock wave and turbulent boundary-layer ...

斜め衝撃波/乱流境界層の3次元干渉場の研究:流れ構造と抽気位置の影響

斜め衝撃波/乱流境界層の3次元干渉場の研究:流れ構造と抽気位置の影響
デジタル文書・図像類
玉山, 雅人, 坂田, 公夫, 柳, 良二, 進藤, 重美, 村上, 哲, 本阿彌, 眞治, Tamayama, Masato, Sakata, Kimio, Yanagi, Ryoji, Shindo, Shigemi, Murakami, Akira, Honami, Shinji航空宇宙技術研究所1994-03航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1227p.1-31
全国の図書館
  • 件名...r bleed effect oblique shock wave flow structure wind tunnel te...
  • 一般注記...to generate an oblique shock wave. The experiments were conduct...

検索結果は以上です。