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

Analytical Investigation on the Underexpanded Jet Issuing from Circular and Elliptic Nozzles
Digital博士論文障害者向け資料あり
Islam Muhammad, Minarul2022-09-26
National Diet Library
  • Subject Heading...t Ratio Nozzle Pressure Ratio
  • Note (General)...ratios, nozzle pressure ratios and design Mach number arbit...

A performance map for ideal air breathing pulse detonation engines [microform] / Daniel E. Paxon ([NASA technical memorandum] ; NASA/TM-2001-211085)

A performance map for ideal air breathing pulse detonation engines [microform] / Daniel E. Paxon ([NASA technical memorandum] ; NASA/TM-2001-211085)
Microform図書
2001<YCA-NAS 1.15:211085>
National Diet Library
  • Subject HeadingAir breathing engines Pulse detonation engines Pressure ratio Detonation Inlet temperature

MECHANISMS AND HAZARD ASSESSMENT OF RAINFALL-INDUCED LANDSLIDE DAMS

MECHANISMS AND HAZARD ASSESSMENT OF RAINFALL-INDUCED LANDSLIDE DAMS
Digital博士論文障害者向け資料あり
Pham, Van Tien2018-03-26
Available onlineNational Diet LibraryOther Libraries in Japan
  • Subject Heading... Critical pore pressure ratio Sliding surface liquefaction

Landslide Hazard Assessment on the Upstream of Dam Reservoir

Landslide Hazard Assessment on the Upstream of Dam Reservoir
Digital博士論文障害者向け資料あり
Hendy, Setiawan2017-03-23
Available onlineNational Diet LibraryOther Libraries in Japan
  • Subject Heading... Critical pore pressure ratio Sliding surface liquefaction

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 Power efficiency

Small engine technology. Task 4, Advanced small turboshaft compressor (ASTC) performance and range investigation [microform] / Jeff L. Hansen and Robert A. Delaney (NASA contractor report ; 198503)

Small engine technology. Task 4, Advanced small turboshaft compressor (ASTC) performance and range investigation [microform] / Jeff L. Hansen and Robert A. Delaney (NASA contractor report ; 198503)
Microform図書
1997<YCA-NAS 1.26:198503>
National Diet Library
  • Subject HeadingTurbomachinery Turboshafts Turbocompressors Pressure ratio Engine design

Coordinates for a high performance 4:1 pressure ratio centrifugal compressor [microform] / Ted F. McKain and Greg J. Holbrook (NASA contractor report ; 204134)

Coordinates for a high performance 4:1 pressure ratio centrifugal compressor [microform] / Ted F. McKain and Greg J. Holbrook (NASA contractor report ; 204134)
Microform図書
1997<YCA-NAS 1.26:204134>
National Diet Library
  • Subject HeadingCentrifugal compressors Pressure ratio Aerodynamics Design analysis ...

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 edges Camber Pressure ratio

Cellular structures in the flow over the flap of a two-element wing [microform] / Steven A. Yon and Joseph Katz ([NASA contractor report] ; 112613)

Cellular structures in the flow over the flap of a two-element wing [microform] / Steven A. Yon and Joseph Katz ([NASA contractor report] ; 112613)
Microform図書
1997<YCA-NAS 1.26:112613>
National Diet Library
  • Subject Heading...ngle of attack Pressure ratio Flow visualization

Analysis of a rocket based combined cycle engine during rocket only operation [microform] / T.D. Smith ... [et al.] (NASA/TM ; 1998-206639/REV1)

Analysis of a rocket based combined cycle engine during rocket only operation [microform] / T.D. Smith ... [et al.] (NASA/TM ; 1998-206639/REV1)
Microform図書
1998<YCA-NAS 1.15:206639/REV 1>
National Diet Library
  • Subject Heading...Rocket engines Pressure ratio Gas generators Ejectors

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)
Microform図書
1996<YCA-NAS 1.26:204473>
National Diet Library
  • Subject Heading...onical nozzles Pressure ratio Noise reduction

Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf [microform] / Milton Lamb and John G. Taylor, Mark C. Frassinelli (NASA technical memorandum ; 4719)

Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf [microform] / Milton Lamb and John G. Taylor, Mark C. Frassinelli (NASA technical memorandum ; 4719)
Microform図書
1996<YCA-NAS 1.15:4719>
National Diet Library
  • Subject HeadingConvergent-divergent nozzles Pressure ratio Pressure distribution Throats...

Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters [microform] / E. Ann Bare and Francis J. Capone (NASA technical memorandum ; 4112)

Static internal performance of convergent single-expansion-ramp nozzles with various combinations of internal geometric parameters [microform] / E. Ann Bare and Francis J. Capone (NASA technical memorandum ; 4112)
Microform図書
1989<YCA-NAS 1.15:4112>
National Diet Library
  • Subject Heading...e distribution Pressure ratio Wind tunnel tests

航技研の推力検定装置について

航技研の推力検定装置について
Digital文書・図像類
小池, 陽, 唐沢, 敏夫, 末永, 尚史, 半沢, 麻雄, 野中, 修, 中谷, 輝臣, 馬場, 滋夫, Koike, Akira, Karasawa, Toshio, Suenaga, Hisashi, Hanzawa, Asao, Nonaka, Osamu, Nakaya, Teruomi, Baba, Sigeo航空宇宙技術研究所2000-07航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory45p.129-135
Other Libraries in Japan
  • Subject Heading...lows transonic pressure ratio interference elimination airt...
  • Note (General)...der to get the pressure ratio equivalent to ...... (1) The sonic pressure ratio, and the pressure ratio equivalent to ......n of transonic pressure ratio. 資料番号: AA0028634013 レポート番号: N...

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

Analytical Investigation on the Underexpanded Jet Issuing from Circular and Elliptic Nozzles
Digital博士論文
Islam Muhammad, Minarul
Available onlineOther Libraries in Japan
  • Summary, etc....ratios, nozzle pressure ratios and design Mach number arbit...
  • Subject Heading...t Ratio Nozzle Pressure Ratio

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