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| 02630cam 2200421zi 4500 |
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| 001 | 9.933067 |
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| 003 | CaOODSP |
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| 005 | 20240216091920 |
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| 006 | m o d f |
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| 007 | cr |n||||||||| |
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| 008 | 240129e199105uuabcad ob f000 0 eng d |
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| 040 | |aCaOODSP|beng|erda|cCaOODSP |
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| 041 | 1 |aeng|bfre |
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| 043 | |an-cn-ab |
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| 086 | 1 |aDR52-6/25-1991E-PDF |
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| 100 | 1 |aBergeron, Maurice Denis, |d1959- |eauthor. |
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| 245 | 12|aA research code to study solutions of the boundary layer equations in body conformal coordinates / |cby Denis Bergeron. |
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| 264 | 1|aRalston, Alberta : |bDefence Research Establishment Suffield : |bNational Defence = Défense nationale, |cMay 1991 |
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| 300 | |a1 online resource (ix, 70, 3, 3, [3] pages) : |billustrations, charts |
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| 336 | |atext|btxt|2rdacontent |
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| 337 | |acomputer|bc|2rdamedia |
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| 338 | |aonline resource|bcr|2rdacarrier |
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| 490 | 1 |aSuffield memorandum ; |vno. 1353 |
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| 500 | |aDigitized edition from print [produced by Defence Research and Development Canada]. |
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| 504 | |aIncludes bibliographical references (pages 69-70). |
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| 520 | 3 |a"The report describes the development of a computer code to solve the two-dimensional boundary layer equations in direct, inverse or mixed direct/inverse mode for airfoil flows. The solution algorithm uses body conformal coordinates and a relaxation scheme with flow-dependent operators. The code incorporates two methods to sweep the flow field. Topics include a description of the code structure, its input requirements, boundary condition and flow field initialization and various software tools required by the main algorithm. Finally, verification results are presented. This work, done in cooperation with the University of Toronto, seeks the development of a boundary layer code compatible with the NASA Ames ARC2D Navier-Stokes code. The two codes will be used in a study of the Fortified Navier-Stokes concept."--abstract (page i). |
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| 546 | |aIncludes abstract in French. |
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| 650 | 0|aBoundary layer|xMathematical models. |
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| 650 | 0|aComputational fluid dynamics. |
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| 650 | 6|aCouche limite|xModèles mathématiques. |
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| 650 | 6|aDynamique des fluides numérique. |
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| 655 | 7|aTechnical reports|2lcgft |
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| 655 | 7|aRapports techniques|2rvmgf |
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| 710 | 2 |aDefence Research Establishment Suffield, |eissuing body. |
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| 710 | 1 |aCanada. |bDepartment of National Defence, |eissuing body. |
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| 830 | #0|aSuffield memorandum ;|vno. 1353.|w(CaOODSP)9.926310 |
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| 856 | 40|qPDF|s3.26 MB|uhttps://publications.gc.ca/collections/collection_2024/rddc-drdc/DR52-6-25-1991-eng.pdf |
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