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| LEADER |
01833cam a2200349 a 4500 |
| 001 |
c000230964 |
| 003 |
CARM |
| 005 |
20070316143420.0 |
| 008 |
900223s1989 onca b f000 0 eng d |
| 015 |
|
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|a C90-70769-0
|
| 019 |
1 |
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|a 6694149
|5 LACONCORD2021
|
| 035 |
|
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|a (OCoLC)21019700
|5 LACONCORD2021
|
| 040 |
|
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|a CAN
|b eng
|c CAN
|d NUN
|d VCAV
|
| 041 |
0 |
|
|a eng
|b fre
|
| 055 |
|
0 |
|a COP.CA.2.1989-2112
|
| 082 |
0 |
4 |
|a 620
|2 20
|
| 100 |
1 |
|
|a Chan, Y. Y.
|
| 245 |
1 |
0 |
|a Analysis of experimental data for CAST 10-2/DOA 2 supercritical airfoil at low Reynolds numbers and application to high Reynolds number flow /
|c by Y.Y. Chan = Analyse des données expérimentales de l'aile supercritique CAST 10-2/DOA 2 aux faibles nombres de Reynolds et application des résultats aux simulations d'écoulement d'air à des nombres de Reynolds élevés / par Y.Y. Chan.
|
| 246 |
3 |
|
|a Analyse des données expérimentales de l'aile supercritique CAST 10-2/DOA 2 aux faibles nombres de Reynolds et application des résultats aux simulations d'écoulement d'air à des nombres de Reynolds élevés
|
| 260 |
|
|
|a Ottawa :
|b National Aeronautical Establishment,
|c 1989.
|
| 300 |
|
|
|a vii, 33 p. :
|b ill. ;
|c 28 cm.
|
| 490 |
1 |
|
|a Aeronautical note ;
|v NAE-AN-60
|
| 500 |
|
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|a "NRC no. 30268".
|
| 504 |
|
|
|a Includes bibliographical references.
|
| 546 |
|
|
|a Text in English only; includes abstract in French.
|
| 650 |
|
0 |
|a Aerofoils.
|
| 650 |
|
0 |
|a Reynolds number.
|
| 710 |
2 |
|
|a National Aeronautical Establishment (Canada)
|
| 830 |
|
0 |
|a Aeronautical note (National Aeronautical Establishment (Canada)) ;
|v NAE-AN-60.
|
| 852 |
8 |
|
|b CARM
|h A1:AP08D0
|i F01593
|p 0352163
|f BK
|
| 999 |
f |
f |
|i d70c45d9-89e5-52ac-9749-398721a5c77c
|s 33f2787a-50f6-573f-8c7c-569e0347ae2c
|
| 952 |
f |
f |
|p Can circulate
|a CAVAL
|b CAVAL
|c CAVAL
|d CARM 1 Store
|e F01593
|f A1:AP08D0
|h Other scheme
|i book
|m 0352163
|