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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
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...t Ratio Nozzle Pressure Ratio
  • 一般注記...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)
マイクロ図書
2001<YCA-NAS 1.15:211085>
国立国会図書館
  • 件名Air 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
デジタル博士論文障害者向け資料あり
Pham, Van Tien2018-03-26
インターネットで読める国立国会図書館全国の図書館
  • 件名... 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
デジタル博士論文障害者向け資料あり
Hendy, Setiawan2017-03-23
インターネットで読める国立国会図書館全国の図書館
  • 件名... 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)
マイクロ図書
2001<YCA-NAS 1.26:210712>
国立国会図書館
  • 件名Wind 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)
マイクロ図書
1997<YCA-NAS 1.26:198503>
国立国会図書館
  • 件名Turbomachinery 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)
マイクロ図書
1997<YCA-NAS 1.26:204134>
国立国会図書館
  • 件名Centrifugal 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)
マイクロ図書
1996<YCA-NAS 1.15:4673>
国立国会図書館
  • 件名Delta 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)
マイクロ図書
1997<YCA-NAS 1.26:112613>
国立国会図書館
  • 件名...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)
マイクロ図書
1998<YCA-NAS 1.15:206639/REV 1>
国立国会図書館
  • 件名...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)
マイクロ図書
1996<YCA-NAS 1.26:204473>
国立国会図書館
  • 件名...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)
マイクロ図書
1996<YCA-NAS 1.15:4719>
国立国会図書館
  • 件名Convergent-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)
マイクロ図書
1989<YCA-NAS 1.15:4112>
国立国会図書館
  • 件名...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
デジタル文書・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
全国の図書館
  • 件名...lows transonic pressure ratio interference elimination airt...
  • 一般注記...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
デジタル博士論文
Islam Muhammad, Minarul
インターネットで読める全国の図書館
  • 要約等...ratios, nozzle pressure ratios and design Mach number arbit...
  • 件名...t Ratio Nozzle Pressure Ratio

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