| NASA Center: |
Langley Research Center |
| Image # : |
L-46802 |
|---|
| Date : |
01/19/1946
|
|---|
|
Title
Wing Flow Method
Full Description
Semispan airplane model and flow-direction vane mounted on wing of P-51D
airplane for transonic tests by wing-flow method.
Keywords
P-51 Mustang Aircraft Scale Models Wings Wing Flow Method Tests Langley NACA
Subject Category
Aeronautical Research, NACA-LaRC,
Reference Numbers
- Center:
LARC
- Center Number:
L-46802
- GRIN DataBase Number:
GPN-2000-001252
Source Information
- Creator/Photographer: UNKNOWN
- Original Source: DIGITAL
| Resolution | Format | Width
(Pixels) | Height
(Pixels) | Size
(KBytes) |
| Thumbnail |
.jpg |
90 |
62 |
7 |
| Small |
.jpg |
640 |
439 |
151 |
| Medium |
.jpg |
1500 |
1029 |
724 |
| Large |
.jpg |
3000 |
2058 |
2,717 |
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Updated Aug 20, 2009
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