Propeller design practical application of the blade element theory - 1 / Fred E. Weick.
This report is the first of a series of four on propeller design and contains a description of the blade element or modified Drzewiecke theory as used in the Bureau of Aeronautics, U. S. Navy Department. Blade interference corrections are used which were taken from R. & M. No. 639 of the British...
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| Main Author: | |
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1926.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
235. |
| Subjects: |
MARC
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| 100 | 1 | |a Weick, Fred E. |0 http://id.loc.gov/authorities/names/n87931046 |1 http://isni.org/isni/000000009789782X. | |
| 245 | 1 | 0 | |a Propeller design practical application of the blade element theory - 1 / |c Fred E. Weick. |
| 260 | |a Washington D.C. : |b National Advisory Committee for Aeronautics, |c 1926. | ||
| 300 | |a 14 pages, 7 unnumbered leaves : |b illustrations, tables ; |c 27 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
| 338 | |a volume |b nc |2 rdacarrier. | ||
| 490 | 1 | |a National Advisory Committee for Aeronautics. Technical Note ; |v no. 235. | |
| 500 | |a "May, 1926." | ||
| 500 | |a NACA TN number 235. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a This report is the first of a series of four on propeller design and contains a description of the blade element or modified Drzewiecke theory as used in the Bureau of Aeronautics, U. S. Navy Department. Blade interference corrections are used which were taken from R. & M. No. 639 of the British Advisory Committee for Aeronautics. The airfoil characteristics used were obtained from tests of model propellers, not from tests of model wings. | |
| 520 | 3 | |a A short method is also shown in which the forces on only one blade element are considered in order to obtain the characteristics of the whole propeller. | |
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| 650 | 0 | |a Propellers |x Design and construction. | |
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| 650 | 7 | |a Propellers, Aerial. |2 fast |0 (OCoLC)fst01079099. | |
| 650 | 7 | |a Propellers |x Design and construction. |2 fast |0 (OCoLC)fst01079091. | |
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