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| LEADER |
01424cam a2200301 a 4500 |
| 001 |
c000230944 |
| 003 |
CARM |
| 005 |
20070316130235.0 |
| 008 |
910603s1990 onca b 000 0 eng d |
| 019 |
1 |
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|a 7942200
|5 LACONCORD2021
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| 035 |
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|a (OCoLC)24777632
|5 LACONCORD2021
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| 040 |
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|a NUN:M
|b eng
|c NUN:M
|d VCAV
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| 041 |
0 |
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|a eng
|b fre
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| 082 |
0 |
4 |
|a 629.13237
|
| 100 |
1 |
|
|a Khalid, M.
|
| 245 |
1 |
0 |
|a Turbulent boundary layer solution for two-dimensional compressible flow using mixing length and K-[epsilon] turbulence models =
|b Résolution du problème des couches limites turbulentes compressibles bidimensionnelles au moyen des modèles de turbulence K-[epsilon] et de longueur de mélange accrue /
|c by M. Khalid.
|
| 260 |
|
|
|a Ottawa :
|b National Research Council Canada,
|c 1990.
|
| 300 |
|
|
|a vi, 31 p. :
|b ill. ;
|c 28 cm.
|
| 490 |
1 |
|
|a Aeronautical note ;
|v IAR-AN-69
|
| 500 |
|
|
|a "NRC NO. 32135"--Cover.
|
| 504 |
|
|
|a Includes bibliographical references.
|
| 546 |
|
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|a Includes summary in French.
|
| 650 |
|
0 |
|a Turbulent boundary layer.
|
| 710 |
2 |
|
|a National Research Council Canada.
|
| 830 |
|
0 |
|a Aeronautical note (National Aeronautical Establishment (Canada)) ;
|v IAR-AN-69.
|
| 852 |
8 |
|
|b CARM
|h A1:AP08D0
|i F01594
|p 0352179
|f BK
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|s 24ac52f9-a5c0-5a37-81fe-b170652d1e8d
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| 952 |
f |
f |
|p Can circulate
|a CAVAL
|b CAVAL
|c CAVAL
|d CARM 1 Store
|e F01594
|f A1:AP08D0
|h Other scheme
|i book
|m 0352179
|