Heat transfer in a turbulent liquid or gas stream / by H. Latzko.
The, theory of heat.transfer from a solid body to a liquid stream could he presented previously only with limiting assumptions about the movement of the fluid (potential flow, laminar frictional flow). (See references 1, 2, and 3)
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| Main Author: | |
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Commitee for Aeronautics,
[1944]
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| Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 1068. |
| Subjects: |
MARC
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| 088 | |a NACA TM 1068 | ||
| 100 | 1 | |a Latzko, H. | |
| 245 | 1 | 0 | |a Heat transfer in a turbulent liquid or gas stream / |c by H. Latzko. |
| 260 | |a Washington, D.C. : |b National Advisory Commitee for Aeronautics, |c [1944] | ||
| 300 | |a 1, 58 pages, 7 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. 1068. | |
| 500 | |a "October 1944." | ||
| 500 | |a NACA TM Number 1068. | ||
| 500 | |a Translated from Zeitschrift fur angewandte Mathematik und Mechanik, Volume 1, Number 4, pp. 268-290, by the National Advisory Commitee for Aeronautics. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a The, theory of heat.transfer from a solid body to a liquid stream could he presented previously only with limiting assumptions about the movement of the fluid (potential flow, laminar frictional flow). (See references 1, 2, and 3) | |
| 520 | 3 | |a For turbulent flow, the most important practical case, the previous theoretical considerations did not go beyond dimensionless formulas and certain conclusions as to the analogy between the friction factor and the unit thermal conductance, (See references 4, 5, 6, and 7,) In order to obtain numerical results, an experimental treatment of the problem was resorted to, which gave rise to numerous investigations because of the importance of this problem in many branches of technology. However, the results of these investigations frequently deviate from one another. The experimental results are especially dependent upon the overall dimensions and the specific proportions of the equipment. | |
| 520 | 3 | |a In the present work, the attempt will be made to develop systematically the theory of the heat transfer and of the dependence of the unit thermal conductance upon shape and dimensions, using as a basis the velocity distribution for turbulent flow set up by Prandtl and Von Karman. | |
| 650 | 0 | |a Heat |x Transmission. |0 http://id.loc.gov/authorities/subjects/sh85059767. | |
| 650 | 0 | |a Turbulence. |0 http://id.loc.gov/authorities/subjects/sh85138753. | |
| 650 | 0 | |a Fluid dynamics. |0 http://id.loc.gov/authorities/subjects/sh85049376. | |
| 650 | 0 | |a Gas dynamics. |0 http://id.loc.gov/authorities/subjects/sh85053291. | |
| 650 | 0 | |a Mathematics. |0 http://id.loc.gov/authorities/subjects/sh85082139. | |
| 650 | 7 | |a Fluid dynamics. |2 fast |0 (OCoLC)fst00927973. | |
| 650 | 7 | |a Gas dynamics. |2 fast |0 (OCoLC)fst00938238. | |
| 650 | 7 | |a Heat |x Transmission. |2 fast |0 (OCoLC)fst00953826. | |
| 650 | 7 | |a Mathematics. |2 fast |0 (OCoLC)fst01012163. | |
| 650 | 7 | |a Turbulence. |2 fast |0 (OCoLC)fst01159210. | |
| 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. 1068. |0 http://id.loc.gov/authorities/names/no2009014150. | |
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