Mathematical and experimental investigation of heat control and power increase in air-cooled aircraft engines / By F. Gosslau.
In order to understand the numerical relations between the air velocity, temperature of the cylinder walls, heat dissipation, cylinder dimensions and type of construction an experimental plant was installed in the Siemens and Halske laboratory. The experimental cylinder was exposed to the air stream...
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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,
[1929]
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| Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 540. |
| Subjects: |
MARC
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| 100 | 1 | |a Gosslau, F. | |
| 245 | 1 | 0 | |a Mathematical and experimental investigation of heat control and power increase in air-cooled aircraft engines / |c By F. Gosslau. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1929] | ||
| 300 | |a 12 pages, 5 unnumbered leaves : |b illustrations ; |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 Technical memorandums ; |v No. 540. | |
| 500 | |a "November, 1929." | ||
| 500 | |a NACA TM Number 540. | ||
| 500 | |a Translated from Zeitschrift fur Flugtechnik.und Motorluftschiffahrt. pp. 461-466, October 7, 1928, by the National Advisory Committee for Aeronautics. | ||
| 520 | 3 | |a In order to understand the numerical relations between the air velocity, temperature of the cylinder walls, heat dissipation, cylinder dimensions and type of construction an experimental plant was installed in the Siemens and Halske laboratory. The experimental cylinder was exposed to the air stream of a wind tunnel. The compression chamber was heated by an electrically heated oil bath kept constantly in motion by a stirrer. The wall temperatures were measured by thermocouples. The air stream was produced a seven-watt blower. The air flowed through a current rectifier (honeycomb), diffuser, air chamber with quieting sieves and a nozzle. | |
| 650 | 0 | |a Airplanes |x Motors |x Cooling. |0 http://id.loc.gov/authorities/subjects/sh85002850. | |
| 650 | 0 | |a Air-cooled engines. |0 http://id.loc.gov/authorities/subjects/sh85002622. | |
| 650 | 0 | |a Airplanes |x Motors |x Cylinders. |0 http://id.loc.gov/authorities/subjects/sh85002852. | |
| 650 | 0 | |a Heat |x Transmission. |0 http://id.loc.gov/authorities/subjects/sh85059767. | |
| 650 | 0 | |a Wind tunnel testing. |0 http://id.loc.gov/authorities/subjects/sh2007008292. | |
| 650 | 7 | |a Air-cooled engines. |2 fast |0 (OCoLC)fst00802334. | |
| 650 | 7 | |a Airplanes |x Motors |x Cooling. |2 fast |0 (OCoLC)fst00803325. | |
| 650 | 7 | |a Airplanes |x Motors |x Cylinders. |2 fast |0 (OCoLC)fst00803328. | |
| 650 | 7 | |a Heat |x Transmission. |2 fast |0 (OCoLC)fst00953826. | |
| 650 | 7 | |a Wind tunnel testing. |2 fast |0 (OCoLC)fst01744047. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://isni.org/isni/0000000106642010. | |
| 830 | 0 | |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ; |v no. 540. |0 http://id.loc.gov/authorities/names/no2009014150. | |
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