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Ten years in the making [microform] : AUSM-family / Meng-Sing Liou ([NASA technical memorandum] ; NASA/TM-2001-210977)

Ten years in the making [microform] : AUSM-family / Meng-Sing Liou ([NASA technical memorandum] ; NASA/TM-2001-210977)
Microform図書
2001<YCA-NAS 1.15:210977>
National Diet Library
  • Subject HeadingComputational fluid dynamics Upwind schemes (Mathematics) Flux differenc...

Factorizable schemes for the equations of fluid flow [microform] / David Sidilkover (ICASE report ; no. 99-20) ([NASA contractor report] ; NASA/CR-1999-209345)

Factorizable schemes for the equations of fluid flow [microform] / David Sidilkover (ICASE report ; no. 99-20) ([NASA contractor report] ; NASA/CR-1999-209345)
Microform図書
1999<YCA-NAS 1.26:209345>
National Diet Library
  • Subject HeadingEuler equations of motion Upwind schemes (Mathematics) Flow equations...

Computational aeroheating predictions for X-34 [microform] / William L. Kleb, Stephen J. Alter (NASA/TM ; 1998-207318)

Computational aeroheating predictions for X-34 [microform] / William L. Kleb, Stephen J. Alter (NASA/TM ; 1998-207318)
Microform図書
1998<YCA-NAS 1.15:207318>
National Diet Library
  • Subject Heading...fluid dynamics Upwind schemes (Mathematics)

Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations [microform] / S. Obayashi and G.P. Guruswamy ([NASA contractor report] ; NASA-CR-203337)

Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations [microform] / S. Obayashi and G.P. Guruswamy ([NASA contractor report] ; NASA-CR-203337)
Microform図書
1995<YCA-NAS 1.26:203337>
National Diet Library
  • Subject Heading...Aeroelasticity Upwind schemes (Mathematics) Steady state C...

An adaptive flow solver for air-borne vehicles undergoing time-dependent motions/deformations [microform] : annual technical progress report, period--August 1, 1996 - July 31, 1997, NASA grant no.--NAG-1-1760 / by Jatinder Singh and Stephen Taylor ([NASA contractor report] ; NASA-CR-205214)

An adaptive flow solver for air-borne vehicles undergoing time-dependent motions/deformations [microform] : annual technical progress report, period--August 1, 1996 - July 31, 1997, NASA grant no.--NAG-1-1760 / by Jatinder Singh and Stephen Taylor ([NASA contractor report] ; NASA-CR-205214)
Microform図書
1997<YCA-NAS 1.26:205214>
National Diet Library
  • Subject Heading... volume method Upwind schemes (Mathematics) Runge-Kutta me...

Parallel Newton-Krylov-Schwarz algorithms for the transonic full potential equation [microform] : NASA contract no. NAS1-19480 / Xiao-Chuan Cai ... [et al.] (ICASE report ; no. 96-39) (NASA contractor report ; 198341)

Parallel Newton-Krylov-Schwarz algorithms for the transonic full potential equation [microform] : NASA contract no. NAS1-19480 / Xiao-Chuan Cai ... [et al.] (ICASE report ; no. 96-39) (NASA contractor report ; 198341)
Microform図書
1996<YCA-NAS 1.26:198341>
National Diet Library
  • Subject Heading...fluid dynamics Upwind schemes (Mathematics) Boundary value...

Wake flow about the Mars Pathfinder entry vehicle [microform] / R.A. Mitcheltree and P.A. Gnoffo (NASA-TM ; 112158)

Wake flow about the Mars Pathfinder entry vehicle [microform] / R.A. Mitcheltree and P.A. Gnoffo (NASA-TM ; 112158)
Microform図書
1995<YCA-NAS 1.15:112158>
National Diet Library
  • Subject Heading...tational grids Upwind schemes (Mathematics)

Application of an upwind high resolution finite-differencing scheme and multigrid method in steady-state incompressible flow simulations [microform] / by Cheng-I Yang ... [et al.]

Application of an upwind high resolution finite-differencing scheme and multigrid method in steady-state incompressible flow simulations [microform] / by Cheng-I Yang ... [et al.]
Microform図書
1996<YCA-NAS 1.15:111216>
National Diet Library
  • Subject HeadingFinite difference theory Upwind schemes (Mathematics) Incompressible...

Application of a third order upwind scheme to viscous flow over clean and iced wings [microform] : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV / A. Bangalore, N. Phaengsook and L.N. Sankar ([NASA contractor report] ; NASA-CR-202616)

Application of a third order upwind scheme to viscous flow over clean and iced wings [microform] : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV / A. Bangalore, N. Phaengsook and L.N. Sankar ([NASA contractor report] ; NASA-CR-202616)
Microform図書
1994<YCA-NAS 1.26:202616>
National Diet Library
  • Subject Heading...e distribution Upwind schemes (Mathematics) Viscous flow A...
  • Alternative TitleApplication of a 3rd order upwind scheme to viscous flow over clean an...
  • Alternative TitleApplication of a 3rd order upwind scheme to viscous flow over clean an...

Computation of separated and unsteady flows with one- and two-equation turbulence models [microform] : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV / J.A. Ekaterinaris and F.R. Menter (NASA-TM ; 111799)

Computation of separated and unsteady flows with one- and two-equation turbulence models [microform] : 32nd Aerospace Sciences meeting & exhibit, January 10-13, 1994/Reno, NV / J.A. Ekaterinaris and F.R. Menter (NASA-TM ; 111799)
Microform図書
1994<YCA-NAS 1.15:111799>
National Diet Library
  • Subject Heading... Unsteady flow Upwind schemes (Mathematics)

Simple algorithms of CFD for compressible flows

Simple algorithms of CFD for compressible flows
Digital文書・図像類
嶋, 英志, Shima, Eiji航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory49Tp.217-223
Other Libraries in Japan
  • Subject Heading...merical scheme upwind scheme advection upstream splitting ...
  • Note (General)...良い結果を与える事を示した。 Upwind scheme is one of the most important ...

HOPE高速飛行実証機の遷音速流解析

HOPE高速飛行実証機の遷音速流解析
Digital文書・図像類
伊藤, 良三, 山本, 行光, Ito, Ryozo, Yamamoto, Yukimitsu航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.187-192
Other Libraries in Japan
  • Subject Heading...on diminishing upwind scheme transonic flow......s equation TVD upwind scheme Reynolds average finite volum...
  • Note (General)...n Diminishing) upwind scheme. The computational grids used...

A solution-adaptive technique using unstructured hexahedral grids

A solution-adaptive technique using unstructured hexahedral grids
Digital文書・図像類
Sun, M., 高山, 和喜, Takayama, Kazuyoshi航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.217-220
Other Libraries in Japan
  • Subject Heading...e second order upwind scheme central differ...... tube monotone upwind scheme
  • Note (General)...USCL (Monotone Upwind Scheme for Conservati......a second-order upwind scheme, and the other employs a seco...

Comparison of effectiveness of four open boundary conditions for incompressible unbounded flows

Comparison of effectiveness of four open boundary conditions for incompressible unbounded flows
Digital文書・図像類
畑山, 茂樹, Hatayama, Shigeki航空宇宙技術研究所1999-01航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1374Tp.1-28
Other Libraries in Japan
  • Subject Heading...is third order upwind scheme high Reynolds number open bou...
  • Note (General)...pe third-order upwind scheme (QUICKEST scheme), and the ef...

Detail of the Leith type third-order of upwind scheme and application to viscous incompressible unbounded flows for Re greater than or equal to 1000

Detail of the Leith type third-order of upwind scheme and application to viscous incompressible unbounded flows for Re greater than or equal to 1000
Digital文書・図像類
畑山, 茂樹, Hatayama, Shigeki航空宇宙技術研究所1999-01航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1373Tp.1-22
Other Libraries in Japan
  • Subject Heading...pe third order upwind scheme high Reynolds number open bou...

CFDは翼型失速角を予測できるか?:乱流モデルの比較

CFDは翼型失速角を予測できるか?:乱流モデルの比較
Digital文書・図像類
松本, 崇, Matsumoto, Takashi航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.123-128
Other Libraries in Japan
  • Subject Heading...ynolds average upwind scheme
  • Note (General)...ence splitting upwind scheme and LU-ADI (Lower Upper-Alter...

近似リーマン解法について:HLLEMスキームの改良と反応流への拡張

近似リーマン解法について:HLLEMスキームの改良と反応流への拡張
Digital文書・図像類
和田, 安弘, Wada, Yasuhiro航空宇宙技術研究所1992-12航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1189p.1-22
Other Libraries in Japan
  • Subject Heading...igh resolution upwind scheme approximate Riemann solver Ri...

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