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Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet [microform] / Michael Papadakis ... [et al.] (NASA/TM-2002-211700)

Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet [microform] / Michael Papadakis ... [et al.] (NASA/TM-2002-211700)
マイクロ図書
2002<YCA-NAS 1.15:2002-211700>
国立国会図書館
  • 件名Water Drops (Liquids) Impingement Airfoils Wings Engine inlets

Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers [microform] / C.J. Steffen, Jr. and J.R. DeBonis ([NASA technical memorandum] ; NASA/TM-1999-209654)

Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers [microform] / C.J. Steffen, Jr. and J.R. DeBonis ([NASA technical memorandum] ; NASA/TM-1999-209654)
マイクロ図書
1999<YCA-NAS 1.15:209654>
国立国会図書館
  • 件名Flow distribution Numerical analysis Engine inlets

Flow through a rectangular-to-semiannular diffusing transition duct [microform] / Jeff Foster ... [et al.] ([NASA contractor report] ; NASA-CR-204816)

Flow through a rectangular-to-semiannular diffusing transition duct [microform] / Jeff Foster ... [et al.] ([NASA contractor report] ; NASA-CR-204816)
マイクロ図書
1997<YCA-NAS 1.26:204816>
国立国会図書館
  • 件名Engine inlets Ducts Ducted flow Flow visual...

IPAC--Inlet Performance Analysis Code [microform] / Paul J. Barnhart ([NASA contractor report] ; NASA CR-204130)

IPAC--Inlet Performance Analysis Code [microform] / Paul J. Barnhart ([NASA contractor report] ; NASA CR-204130)
マイクロ図書
1997<YCA-NAS 1.26:204130>
国立国会図書館
  • 件名...ery Inlet flow Engine inlets Reliability analysis Aerodyna...

Finite difference time marching in the frequency domain [microform] : a parabolic formulation for aircraft acoustic nacelle design / Kenneth J. Baumeister and Kevin L. Kreider (NASA technical memorandum ; 106839)

Finite difference time marching in the frequency domain [microform] : a parabolic formulation for aircraft acoustic nacelle design / Kenneth J. Baumeister and Kevin L. Kreider (NASA technical memorandum ; 106839)
マイクロ図書
1996<YCA-NAS 1.15:106839>
国立国会図書館
  • 件名Finite difference theory Time marching Nacelles Sound propagation Aircraft engines Engine inlets

Comparison of the aeroacoustics of two small-scale supersonic inlets [microform] : final technical report, NASA contract #--NAG 3-1539 / principal investigator, Wing Ng ([NASA contractor report] ; 206507)

Comparison of the aeroacoustics of two small-scale supersonic inlets [microform] : final technical report, NASA contract #--NAG 3-1539 / principal investigator, Wing Ng ([NASA contractor report] ; 206507)
マイクロ図書
1996<YCA-NAS 1.26:206507>
国立国会図書館
  • 件名...ersonic inlets Engine inlets Aircraft engines Flow distrib...

Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 [microform] / Saied Enami ... [et al.] (NASA technical paper ; 3502)

Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4 [microform] / Saied Enami ... [et al.] (NASA technical paper ; 3502)
マイクロ図書
1995<YCA-NAS 1.60:3502>
国立国会図書館
  • 件名Combustion chambers Engine inlets Isolators Performance tests S...

Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow [microform] / Kenneth J. Baumeister and Kevin L. Kreider (NASA technical memorandum ; 107363)

Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow [microform] / Kenneth J. Baumeister and Kevin L. Kreider (NASA technical memorandum ; 107363)
マイクロ図書
1996<YCA-NAS 1.15:107363>
国立国会図書館
  • 件名...time operation Engine inlets Ducted flow Iterative solutio...

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis (NASA technical memorandum ; 110300)

A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 [microform] / Richard J. Re and William K. Abeyounis (NASA technical memorandum ; 110300)
マイクロ図書
1996<YCA-NAS 1.15:110300>
国立国会図書館
  • 件名...tatic pressure Engine inlets Aircraft engines Mach number ...

Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach [microform] / W.P. Norby, J.A. Ladd, and A.J. Yuhas (NASA contractor report ; 198053)

Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach [microform] / W.P. Norby, J.A. Ladd, and A.J. Yuhas (NASA contractor report ; 198053)
マイクロ図書
1996<YCA-NAS 1.26:198053>
国立国会図書館
  • 件名...bulence models Engine inlets Computational grids Flow dist...

Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems [microform] (<v.1>: NASA contractor report ; 195480) (<v.2>: NASA contractor report ; NASA CR-202309)

Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems [microform] (<v.1>: NASA contractor report ; 195480) (<v.2>: NASA contractor report ; NASA CR-202309)
マイクロ図書
1996<YCA-NAS 1.26:195480>
国立国会図書館
  • 件名...puter programs Engine inlets Engine noise Noise prediction...

Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations [microform] : a final technical report for NASA-LeRC grant NAG-1781 / David A. Boger, T.R. Govindan, and Henry McDonald ([NASA contractor report] ; NASA CR-206334)

Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations [microform] : a final technical report for NASA-LeRC grant NAG-1781 / David A. Boger, T.R. Govindan, and Henry McDonald ([NASA contractor report] ; NASA CR-206334)
マイクロ図書
1997<YCA-NAS 1.26:206334>
国立国会図書館
  • 件名...rbulence model Engine inlets Predictions Aircraft engines ...

Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster (NASA technical memorandum ; 107274) (ICOMP ; 96-6)

Rocket-based combined cycle engine technology development [microform] : inlet CFD validation and application / J.R. DeBonis and S. Yungster (NASA technical memorandum ; 107274) (ICOMP ; 96-6)
マイクロ図書
1996<YCA-NAS 1.15:107274>
国立国会図書館
  • 件名...Rocket engines Engine inlets Navier-Stokes equation Comput...

Improved finite element modeling of the turbofan engine inlet radiation problem [microform] / Indranil Danda Roy and Walter Eversman, H.D. Meyer ([NASA contractor report] ; NASA-CR-204341)

Improved finite element modeling of the turbofan engine inlet radiation problem [microform] / Indranil Danda Roy and Walter Eversman, H.D. Meyer ([NASA contractor report] ; NASA-CR-204341)
マイクロ図書
1993<YCA-NAS 1.26:204341>
国立国会図書館
  • 件名...rbofan engines Engine inlets Mathematical models Digital s...

Fan noise prediction system development [microform] : source/radiation field coupling and workstation conversion for the acoustic radiation code / H.D. Meyer ([NASA contractor report] ; NASA-CR-204340)

Fan noise prediction system development [microform] : source/radiation field coupling and workstation conversion for the acoustic radiation code / H.D. Meyer ([NASA contractor report] ; NASA-CR-204340)
マイクロ図書
1993<YCA-NAS 1.26:204340>
国立国会図書館
  • 件名Aerodynamic noise Engine inlets Finite element method Acousti...

航技研におけるガスタービンおよびジェットエンジン燃焼器研究開発

航技研におけるガスタービンおよびジェットエンジン燃焼器研究開発
デジタル文書・図像類
田丸, 卓, Tamaru, Takashi航空宇宙技術研究所1995-01航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory676p.1-113
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