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Effect of delta tabs on free jets from complex nozzles [microform] / K.B.M.Q Zaman ([NASA technical memorandum] ; NASA/TM-2001-210674)

Effect of delta tabs on free jets from complex nozzles [microform] / K.B.M.Q Zaman ([NASA technical memorandum] ; NASA/TM-2001-210674)
Microform図書
2001<YCA-NAS 1.15:210674>
National Diet Library
  • Subject HeadingEjectors Flow distribution Free jets Nozzle flow Simulation Tabs (Control surf...

Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations [microform] / Kevin L. Mikkelsen and Timothy J. McDonald ; [prepared under contract NAS3-98021] ([NASA contractor report] ; NASA/CR-2001-210712)

Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations [microform] / Kevin L. Mikkelsen and Timothy J. McDonald ; [prepared under contract NAS3-98021] ([NASA contractor report] ; NASA/CR-2001-210712)
Microform図書
2001<YCA-NAS 1.26:210712>
National Diet Library
  • Subject HeadingWind tunnel tests Cold flow tests Nozzle flow Pressure ratio static tests P...

An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code [microform] / Mary Ann Dembowski and Nicholas J. Georgiadis (NASA/TM-2002-211727)

An evaluation of parameters influencing jet mixing using the WIND Navier-Stokes Code [microform] / Mary Ann Dembowski and Nicholas J. Georgiadis (NASA/TM-2002-211727)
Microform図書
2002<YCA-NAS 1.15:2002-211727>
National Diet Library
  • Subject Heading...tokes equation Nozzle flow Turbulence models Turbulent m...

First NASA/Industry High Speed Research Program Nozzle Symposium [microform] / proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, November 17-19, 1992 ([NASA conference publication] ; NASA/CP-1999-209423)

First NASA/Industry High Speed Research Program Nozzle Symposium [microform] / proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, November 17-19, 1992 ([NASA conference publication] ; NASA/CP-1999-209423)
Microform図書
1999<YCA-NAS 1.55:209423>
National Diet Library
  • Subject HeadingConferences Low noise Nozzle design Nozzle flow Nozzle efficiency Technology ...

Design and checkout of a high speed research nozzle evaluation rig [microform] / Raymond S. Castner, John D. Wolter (NASA technical memorandum ; 113179)

Design and checkout of a high speed research nozzle evaluation rig [microform] / Raymond S. Castner, John D. Wolter (NASA technical memorandum ; 113179)
Microform図書
1997<YCA-NAS 1.15:113179>
National Diet Library
  • Subject HeadingHigh speed Nozzle flow Design analysis Evaluation Sc...

A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields [microform] / Nicholas J. Georgiadis, Dennis A. Yoder, and James R. DeBonis (NASA/TM ; 1999-209184)

A comparison of three Navier-Stokes solvers for exhaust nozzle flowfields [microform] / Nicholas J. Georgiadis, Dennis A. Yoder, and James R. DeBonis (NASA/TM ; 1999-209184)
Microform図書
1999<YCA-NAS 1.15:209184>
National Diet Library
  • Subject Heading...tokes equation Nozzle flow Turbulent mixing
  • Alternative TitleComparison of three Navier Stokes solvers for exhaust nozzle flowfields
  • Alternative TitleComparison of three Navier Stokes solvers for exhaust nozzle flowfields

Three dimensional viscous flow field in an axial flow turbine nozzle passage [microform] / D. Risti'c and B. Lakshminarayana (NASA contractor report ; 4779)

Three dimensional viscous flow field in an axial flow turbine nozzle passage [microform] / D. Risti'c and B. Lakshminarayana (NASA contractor report ; 4779)
Microform図書
1997<YCA-NAS 1.26:4779>
National Diet Library
  • Subject Heading...w Viscous flow Nozzle flow Aerodynamic characteristics C...

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)
Microform図書
1999<YCA-NAS 1.60:209093>
National Diet Library
  • Subject Heading...d tunnel tests Nozzle flow Oblique shock waves Flow visu...

Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application [microform] / Jack (Jagdish) S. Sokhey and Baily R. Vittal, David W. Lam (NASA technical memorandum ; 113181)

Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application [microform] / Jack (Jagdish) S. Sokhey and Baily R. Vittal, David W. Lam (NASA technical memorandum ; 113181)
Microform図書
1997<YCA-NAS 1.15:113181>
National Diet Library
  • Subject HeadingExhaust nozzles Nozzle flow Powered lift aircraft Vertica...

Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability [microform] / David J. Wing, Charles T.L. Mills, and Mary L. Mason (NASA techical paper ; 3628)

Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability [microform] / David J. Wing, Charles T.L. Mills, and Mary L. Mason (NASA techical paper ; 3628)
Microform図書
1997<YCA-NAS 1.60:3628>
National Diet Library
  • Subject Heading...ergent nozzles Nozzle flow Transonic wind tunnels Static...

Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section [microform] / P.W. Giel ... [et al.] (NASA technical memorandum ; 107284) (Army Research Laboratory memorandum report ; ARL-MR-152)

Three-dimensional Navier-Stokes analysis and redesign of an imbedded bellmouth nozzle in a turbine cascade inlet section [microform] / P.W. Giel ... [et al.] (NASA technical memorandum ; 107284) (Army Research Laboratory memorandum report ; ARL-MR-152)
Microform図書
1996<YCA-NAS 1.15:107284>
National Diet Library
  • Subject Heading...n Cascade flow Nozzle flow Flow geometry

Advanced space propulsion system flowfield modeling [microform] : final report : contract NAS8-40845 / by Sheldon D. Smith ([NASA contractor report] ; NASA/CR-208195 [i.e. 208864])

Advanced space propulsion system flowfield modeling [microform] : final report : contract NAS8-40845 / by Sheldon D. Smith ([NASA contractor report] ; NASA/CR-208195 [i.e. 208864])
Microform図書
1998<YCA-NAS 1.26:208195>
National Diet Library
  • Subject HeadingNozzle flow Boundary layer flow Mathemati...

Numerical analysis of base flowfield for a four-engine clustered nozzle configuration [microform] / T.-S. Wang (NASA-TM ; 112304)

Numerical analysis of base flowfield for a four-engine clustered nozzle configuration [microform] / T.-S. Wang (NASA-TM ; 112304)
Microform図書
1995<YCA-NAS 1.15:112304>
National Diet Library
  • Subject Heading... Base pressure Nozzle flow

Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury (NASA technical paper ; 3440)

Two-dimensional converging-diverging rippled nozzles at transonic speeds [microform] / John R. Carlson and Scott C. Asbury (NASA technical paper ; 3440)
Microform図書
1994<YCA-NAS 1.60:3440>
National Diet Library
  • Subject Heading...efficient Drag Nozzle flow Nozzle geometry Thrust Traili...

Comparison of turbulence models for nozzle-afterbody flows with propulsive jets [microform] / William B. Compton III (NASA techical paper ; 3592)

Comparison of turbulence models for nozzle-afterbody flows with propulsive jets [microform] / William B. Compton III (NASA techical paper ; 3592)
Microform図書
1996<YCA-NAS 1.60:3592>
National Diet Library
  • Subject Heading...tokes equation Nozzle flow Turbulence models K-Epsilon t...

超音速エンジン風洞における風洞始動荷重

超音速エンジン風洞における風洞始動荷重
Digital文書・図像類
櫻中, 登, 志村, 隆, 三谷, 徹, 泉川, 宗男, 富岡, 定毅, 平岩, 徹夫, Sakuranaka, Noboru, Simura, Takashi, Mitani, Toru, Izumikawa, Muneo, Tomioka, Sadatake, Hiraiwa, Tetsuo航空宇宙技術研究所1998-10航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1360p.1-21
Other Libraries in Japan
  • Subject Heading...ure supersonic nozzle flow
  • Note (General)...cture in which nozzle flow is recompressed by a separati...

スクラムジェットの着火におよぼす蓄熱体加熱器からの粉塵の影響

スクラムジェットの着火におよぼす蓄熱体加熱器からの粉塵の影響
Digital文書・図像類
三谷, 徹, Mitani, Toru航空宇宙技術研究所1994-04航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1234p.1-17
Other Libraries in Japan
  • Subject Heading...e distribution nozzle flow mass fraction wind tunnel tes...

スクラムジェットにおける化学反応:簡略化反応系による考察

スクラムジェットにおける化学反応:簡略化反応系による考察
Digital文書・図像類
三谷, 徹, Mitani, Toru航空宇宙技術研究所1992-11航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1184p.1-29
Other Libraries in Japan
  • Subject Heading... flow reactive nozzle flow chemical reaction process com...
  • Alternative Title...combustion and nozzle flow
  • Alternative Title...combustion and nozzle flow

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