Some problems of the calculation of three-dimensional boundary-layer flows on general configurations

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050 ⊔ 4 ‡aTL521.3.C6 ‡bA3 no. 2285
245 0 0 ‡aSome problems of the calculation of three-dimensional boundary-layer flows on general configurations / ‡cby Tuncer Cebeci ... [et al.].
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1973.
300 ⊔ ⊔ ‡avi, 52 p. : ‡bill. ; ‡c27 cm.
490 ⊔ 0 ‡aNASA contractor report ; ‡vNASA CR-2285
500 ⊔ ⊔ ‡a"Prepared by Douglas Aircraft Company, McDonnell Douglas Corporation ... for Langley Research Center."
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aBibliography: p. 50-52.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 0 7 ‡aTurbulente Grenzschicht. ‡2swd
650 0 7 ‡aDreidimensionale Strömung. ‡2swd
650 ⊔ 0 ‡aFluid dynamics ‡xMathematical models.
650 ⊔ 0 ‡aTurbulence ‡xMathematical models.
650 ⊔ 0 ‡aBoundary layer ‡xMathematical models.
700 1 ⊔ ‡aCebeci, Tuncer.
710 2 ⊔ ‡aLangley Research Center.
710 2 ⊔ ‡aDouglas Aircraft Company.
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DAT 1 ⊔ ‡a20141112173021.0 ‡b2024-01-19T18:53:50Z
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