Design charts for cross-flow tubular intercoolers charge-through-tube type / by J. George Reuter and Michael F. Valerino.
On the basis of current heat-transfer theory, equations are developed relating the various dimensions, the air weight flow, and the performance of a cross-flow tubular intercooler in which the charge flows through and the cooling air across the tubes. These equations are then presented in graphical...
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| Corporate Authors: | , |
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| Other title: | NACA Wartime Reports. Series E. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1941]
|
| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. E106. |
| Subjects: |
MARC
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| 086 | 0 | |a Y 3.N 21/5:11/E106 | |
| 088 | |a NACA WR E106 | ||
| 100 | 1 | |a Reuter, J. George. | |
| 245 | 1 | 0 | |a Design charts for cross-flow tubular intercoolers charge-through-tube type / |c by J. George Reuter and Michael F. Valerino. |
| 246 | 3 | |a NACA Wartime Reports. Series E. | |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c [1941] | ||
| 300 | |a 35 pages, 10 unnumbered pages : |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 Wartime Report / National Advisory Committee for Aeronautics ; |v no. E106. | |
| 500 | |a NACA Wartime Report E-106. | ||
| 500 | |a Originally issued as NACA as an Advance Confidential Report (July 1941) | ||
| 500 | |a Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a On the basis of current heat-transfer theory, equations are developed relating the various dimensions, the air weight flow, and the performance of a cross-flow tubular intercooler in which the charge flows through and the cooling air across the tubes. These equations are then presented in graphical form in a series of design charts from which the intercooler design characteristics and performance can be quickly determined. A method of determining and presenting the performance of a given intercooler at various operating conditions is indicated. | |
| 650 | 0 | |a Airplanes |x Motors |x Cooling. |0 http://id.loc.gov/authorities/subjects/sh85002850. | |
| 650 | 0 | |a Internal combustion engines |x Cooling. |0 http://id.loc.gov/authorities/subjects/sh85067317. | |
| 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 Charts, diagrams, etc. |0 http://id.loc.gov/authorities/subjects/sh87002373. | |
| 650 | 0 | |a Mathematics. |0 http://id.loc.gov/authorities/subjects/sh85082139. | |
| 650 | 7 | |a Airplanes |x Motors |x Cooling. |2 fast |0 (OCoLC)fst00803325. | |
| 650 | 7 | |a Charts, diagrams, etc. |2 fast |0 (OCoLC)fst00852545. | |
| 650 | 7 | |a Heat |x Transmission. |2 fast |0 (OCoLC)fst00953826. | |
| 650 | 7 | |a Internal combustion engines |x Cooling. |2 fast |0 (OCoLC)fst00976520. | |
| 650 | 7 | |a Mathematics. |2 fast |0 (OCoLC)fst01012163. | |
| 650 | 7 | |a Tubes. |2 fast |0 (OCoLC)fst01158581. | |
| 700 | 1 | |a Valerino, Michael F. | |
| 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. | |
| 710 | 2 | |a Aircraft Engine Research Laboratory. |0 http://id.loc.gov/authorities/names/no2006105898. | |
| 830 | 0 | |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ; |v no. E106. | |
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| 952 | f | f | |p Can circulate |a University of Colorado Boulder |b Boulder Campus |c Norlin |d Norlin Library - Basement - Government Information - US |e Y 3.N 21/5:11/E106 |h Superintendent of Documents classification |i document |m U183073195507 |n 1 |