| Description: | The 6-foot-4-inch wind tunnel and its auxiliary equipment has proven itself capable of continuous and reliable output of data. The real value of the tunnel will increase as experience is gained in checking the observed tunnel performance against full-scale performance. Such has been the case of the 8- by 8-foot tunnel, and for that reason the comparison in the calibration tests have been presented. |
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| Creator(s): | |
| Creation Date: | August 1, 1935 |
| Partner(s): |
UNT Libraries Government Documents Department
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| Collection(s): |
National Advisory Committee for Aeronautics Collection
Technical Report Archive and Image Library
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| Usage: |
Total Uses: 126
Past 30 days: 8
Yesterday: 0
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| Creator (Author): | ||
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| Creator (Author): | ||
| Original Creation Date: | August 1, 1935 | |
| Description: | The 6-foot-4-inch wind tunnel and its auxiliary equipment has proven itself capable of continuous and reliable output of data. The real value of the tunnel will increase as experience is gained in checking the observed tunnel performance against full-scale performance. Such has been the case of the 8- by 8-foot tunnel, and for that reason the comparison in the calibration tests have been presented. |
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| Serial Title: | NACA Technical Notes | |
| Partner: |
UNT Libraries Government Documents Department
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| Collection: |
National Advisory Committee for Aeronautics Collection
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| Collection: |
Technical Report Archive and Image Library
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| Identifier: |
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| Resource Type: | Report | |
| Format: | Text | |
| Rights: |
Access:
Public
License:
Public Domain
Statement:
No Copyright, Unclassified, Unlimited, Publicly available
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