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検索結果 148 件

Decomposing solid micropropulsion nozzle performance issues [microform] / Brian Reed (NASA/TM-2003-212225)

Decomposing solid micropropulsion nozzle performance issues [microform] / Brian Reed (NASA/TM-2003-212225)
マイクロ図書
2003<YCA-NAS 1.15:212225>
国立国会図書館
  • 件名...tion Thrustors Nozzle design Nozzle geometry Nozzle efficiency

臨界ノズル : 測定原理から新しい問題まで

臨界ノズル : 測定原理から新しい問題まで
紙図書
中尾晨一 著日刊工業新聞社2017.4<M191-L73>
国立国会図書館全国の図書館
  • 典拠情報（件名/「を見よ」参照）流量測定 流量計 流速計 Flow meters Nozzles
  • 並列タイトル等（連結）Critical Flow Venturi Nozzles
  • 並列タイトル等Critical Flow Venturi Nozzles

Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility [microform] / Kin C. Wong (NASA/TM-2003-212326)

Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility [microform] / Kin C. Wong (NASA/TM-2003-212326)
マイクロ図書
2003<YCA-NAS 1.15:212326>
国立国会図書館
  • 件名...rement Exhaust nozzles Nozzle geometry Calibrating

Separate flow nozzle test status meeting [microform] : proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997 / [Naseem H. Saiyed, editor] ([NASA conference publication] ; NASA/CP-2000-210524)

Separate flow nozzle test status meeting [microform] : proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997 / [Naseem H. Saiyed, editor] ([NASA conference publication] ; NASA/CP-2000-210524)
マイクロ図書
2000<YCA-NAS 1.55:210524>
国立国会図書館
  • 件名Jet aircraft noise Engine noise Acoustic nozzles Aeroacoustics Sonic nozzles Exhaust nozzles

A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications [microform] / Rickey J. Shyne (NASA/TM-2002-211977)

A survey of challenges in aerodynamic exhaust nozzle technology for aerospace propulsion applications [microform] / Rickey J. Shyne (NASA/TM-2002-211977)
マイクロ図書
2002<YCA-NAS 1.15:2002-211977>
国立国会図書館
  • 件名Nozzles Aerodynamics Propulsion

Analytical Investigation on the Underexpanded Jet Issuing from Circular and Elliptic Nozzles

Analytical Investigation on the Underexpanded Jet Issuing from Circular and Elliptic Nozzles
デジタル博士論文障害者向け資料あり
Islam Muhammad, Minarul2022-09-26
国立国会図書館
  • 件名...n Aspect Ratio Nozzle Pressure Ratio
  • 一般注記...gent-divergent nozzle has been inves......aspect ratios, nozzle pressure ratios and design Ma...

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)
マイクロ図書
1999<YCA-NAS 1.55:209423>
国立国会図書館
  • 件名Conferences Low noise Nozzle design Nozzle flow Nozzle efficiency Technology assessm...
  • 並列タイトル等（連結）...search Program Nozzle Symposium NASA......search Program Nozzle Symposium
  • 並列タイトル等...search Program Nozzle Symposium NASA......search Program Nozzle Symposium

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)
マイクロ図書
2002<YCA-NAS 1.15:2002-211727>
国立国会図書館
  • 件名...tokes equation Nozzle flow Turbulenc......ing Supersonic nozzles Application programs (Comput...

AST critical propulsion and noise reduction technologies for future commercial subsonic engines [microform] : separate-flow exhaust system noise reduction concept evaluation / B.A. Janardan ... [et al.] ([NASA contractor report] ; NASA/CR-2000-210039)

AST critical propulsion and noise reduction technologies for future commercial subsonic engines [microform] : separate-flow exhaust system noise reduction concept evaluation / B.A. Janardan ... [et al.] ([NASA contractor report] ; NASA/CR-2000-210039)
マイクロ図書
2000<YCA-NAS 1.26:210039>
国立国会図書館
  • 件名Acoustic nozzles Aeroacoustics Engine noise Jet aircraft noise Noise reduction Sonic nozzles

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Convergent-divergent nozzles Boundary laye......on Wind tunnel nozzles Wind tunnel tests Nozzle flow Oblique shock waves Flow...

Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle [microform] / Michael K. Ponton, John M. Seiner, and Martha C. Brown (NASA technical memorandum ; 113137)

Near field pressure fluctuations in the exit plane of a choked axisymmetric nozzle [microform] / Michael K. Ponton, John M. Seiner, and Martha C. Brown (NASA technical memorandum ; 113137)
マイクロ図書
1997<YCA-NAS 1.15:113137>
国立国会図書館
  • 件名Sonic nozzles Transonic nozzles Supersonic nozzles Pressure oscillations Flame ...

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle [microform] / Karen A. Deere and Scott C. Asbury (NASA/TP ; 1999-209138)

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle [microform] / Karen A. Deere and Scott C. Asbury (NASA/TP ; 1999-209138)
マイクロ図書
1999<YCA-NAS 1.60:209138>
国立国会図書館
  • 件名...hroats Exhaust nozzles Nozzle design Computa......rbulence model Nozzle efficiency

Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure [microform] / Robert S. Jankovsky and John M. Kazaroff, Albert J. Pavli (NASA techical paper ; 3576)

Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure [microform] / Robert S. Jankovsky and John M. Kazaroff, Albert J. Pavli (NASA techical paper ; 3576)
マイクロ図書
1996<YCA-NAS 1.60:3576>
国立国会図書館
  • 件名Rocket nozzles Exhaust veloc......ecific impulse Nozzle thrust coefficients Nozzle geometry Thrus......amber pressure Nozzle efficiency Divergent nozzles
  • 並列タイトル等（連結）Experimental performance of a high area ratio rocket nozzle at high combustion chamber pr...
  • 並列タイトル等Experimental performance of a high area ratio rocket nozzle at high combustion chamber pr...

Computing axisymmetric jet screech tones using unstructured grids [microform] / Philip C.E. Jorgenson, Ching Y. Loh ; prepared for the 38th Joint Propulsion Conference and Exhibit sponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002 (NASA/TM-2002-211799)

Computing axisymmetric jet screech tones using unstructured grids [microform] / Philip C.E. Jorgenson, Ching Y. Loh ; prepared for the 38th Joint Propulsion Conference and Exhibit sponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002 (NASA/TM-2002-211799)
マイクロ図書
2002<YCA-NAS 1.15:211799>
国立国会図書館
  • 件名Unstructured grids Screech tones Aeroacoustics Axisymmetric flow Nozzle geometry

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)
マイクロ図書
1999<YCA-NAS 1.15:209184>
国立国会図書館
  • 件名...ectors Exhaust nozzles Flow characte......tokes equation Nozzle flow Turbulent mixing
  • 並列タイトル等（連結）Comparison of three Navier Stokes solvers for exhaust nozzle flowfields
  • 並列タイトル等Comparison of three Navier Stokes solvers for exhaust nozzle flowfields

Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing ([NASA technical paper] ; NASA/TP-1998-206912)

Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct [microform] / David J. Wing ([NASA technical paper] ; NASA/TP-1998-206912)
マイクロ図書
1998<YCA-NAS 1.60:206912>
国立国会図書館
  • 件名Thrust vector control Nozzle geometry Convergent nozzles Angular distribution Flow di...

Computational noise study of a supersonic short conical plug-nozzle jet [microform] / Indu S. Das, Abbas Khavaran, and A.P. Das (NASA contractor report ; NASA-CR-204473)

Computational noise study of a supersonic short conical plug-nozzle jet [microform] / Indu S. Das, Abbas Khavaran, and A.P. Das (NASA contractor report ; NASA-CR-204473)
マイクロ図書
1996<YCA-NAS 1.26:204473>
国立国会図書館
  • 件名Plug nozzles Supersonic nozzles Aeroacoustics...... noise Conical nozzles Pressure ratio Noise reducti...

Multidisciplinary approach to aerospike nozzle design [microform] / J.J. Korte ... [et al.] (NASA technical memorandum ; 110326)

Multidisciplinary approach to aerospike nozzle design [microform] / J.J. Korte ... [et al.] (NASA technical memorandum ; 110326)
マイクロ図書
1997<YCA-NAS 1.15:110326>
国立国会図書館
  • 件名Nozzle design Engine ...... method Rocket nozzles

CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system [microform] : final report : under contract NAG3-1500 / Ing Chuang, Louis G. Hunter ([NASA contractor report] ; NASA-CR-202418)

CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system [microform] : final report : under contract NAG3-1500 / Ing Chuang, Louis G. Hunter ([NASA contractor report] ; NASA-CR-202418)
マイクロ図書
1997<YCA-NAS 1.26:202418>
国立国会図書館
  • 件名Nozzle thrust coeffic...... Inviscid flow Nozzle walls Nozzle geometry Engine design Comput...

Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure [microform] / M. Moin Hussaini and John J. Korte (NASA technical memorandum ; 110295)

Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure [microform] / M. Moin Hussaini and John J. Korte (NASA technical memorandum ; 110295)
マイクロ図書
1996<YCA-NAS 1.15:110295>
国立国会図書館
  • 件名...tokes equation Nozzle design Rocket nozzles Low Reynolds number Nozzle thrust coefficients
  • 並列タイトル等（連結）Investigation of low Reynolds number rocket nozzle design using PNS-based optimi...
  • 並列タイトル等Investigation of low Reynolds number rocket nozzle design using PNS-based optimi...