Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages / Robert G. Diessler.
A previous analysis for fully developed turbulent heat transfer and flow with variable fluid properties is extended and applied to the entrance regions of smooth tubes and parallel flat plates. Integral heat-transfer and momentum equations are used for calculating the thicknesses of the thermal and...
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| Other title: | Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1953.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3016. |
| Subjects: |
MARC
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| 100 | 1 | |a Diessler, Robert G. | |
| 245 | 1 | 0 | |a Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages / |c Robert G. Diessler. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1953. | ||
| 300 | |a 88 pages : |b illustrations ; |c 28 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
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| 490 | 1 | |a National Advisory Committee for Aeronautics. Technical Note ; |v no. 3016. | |
| 500 | |a "October 1953." | ||
| 500 | |a NACA TN Number 3016. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a A previous analysis for fully developed turbulent heat transfer and flow with variable fluid properties is extended and applied to the entrance regions of smooth tubes and parallel flat plates. Integral heat-transfer and momentum equations are used for calculating the thicknesses of the thermal and flow boundary layers. The effect of variable properties is determined for the case of uniform heat flux, uniform initial temperature distribution, and fully developed velocity distribution. A number of ther cases in which the fluid properties are considered constant are analyzed. The predicted Nusselt numbers for air with a uniform wall temperature and uniform initial temperature and velocity distributions agree closely with experimentally determined values. | |
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| 650 | 0 | |a Air flow. |0 http://id.loc.gov/authorities/subjects/sh85002635. | |
| 650 | 0 | |a Tubes. |0 http://id.loc.gov/authorities/subjects/sh85138452. | |
| 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. | |
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| 730 | 0 | |a Technical report archive and image library. |0 http://id.loc.gov/authorities/names/no2008179973. | |
| 776 | 0 | 8 | |i Online version: |a Diessler, Robert G. |t Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages. |d Washington, D.C. : National Advisory Committee for Aeronautics, 1953 |w (OCoLC)885174682. |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 3016. |0 http://id.loc.gov/authorities/names/no2009017392. | |
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