The use of hot-film technique for boundary layer studies on a 21% thick airfoil = Utilisation de la technique du film chaud pour des études de couche limite autour d'un profil d'aile d'une épaisseur relative de 21% /
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| Main Author: | |
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| Corporate Authors: | , |
| Format: | Book |
| Language: | English |
| Published: |
Ottawa :
National Research Council Canada,
1987.
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| Series: | Aeronautical note (National Aeronautical Establishment (Canada)) ;
NAE-AN-45 |
| Subjects: |
CARM 1 Store
| Call Number: |
A2:AI22H0 F01602 |
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| Copy 1 | Available Place a Hold |