| Description: | This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 A, U.S.A. 35 B, Clark Y, R.A.F. 15, and Gottingen 387, as determined at various Reynolds numbers up to an approximately full scale value in the variable density wind tunnel of the National Advisory Committee for Aeronautics. It is shown that the characteristics of the wings investigated are affected greatly and in a somewhat erratic manner by variation of the Reynolds number. In general there is a small increase in maximum lift and an appreciable decrease in drag at all lifts. |
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| Creator(s): | |
| Creation Date: | January 1, 1927 |
| 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: 62
Past 30 days: 4
Yesterday: 0
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| Creator (Author): | ||
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| Creator (Author): | ||
| Original Creation Date: | January 1, 1927 | |
| Description: | This report contains the aerodynamic properties of the wing sections U.S.A. 5, U.S.A. 27, U.S.A. 35 A, U.S.A. 35 B, Clark Y, R.A.F. 15, and Gottingen 387, as determined at various Reynolds numbers up to an approximately full scale value in the variable density wind tunnel of the National Advisory Committee for Aeronautics. It is shown that the characteristics of the wings investigated are affected greatly and in a somewhat erratic manner by variation of the Reynolds number. In general there is a small increase in maximum lift and an appreciable decrease in drag at all lifts. |
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| Serial Title: | NACA Technical Reports | |
| 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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