Turbulence and heat stratification / by H. Schlichting.
With applications to meteorology in view, the method of small oscillations is used to investigate the stability of a plane laminar boundary layer in which the density depends in a special way on the distance from the plate. It is found that for a constant Froude number the flow becomes more stable a...
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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,
[1950]
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Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 1262. |
Subjects: |
MARC
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245 | 1 | 0 | |a Turbulence and heat stratification / |c by H. Schlichting. |
260 | |a Washington, D.C. : |b National Advisory Commitee for Aeronautics, |c [1950] | ||
300 | |a 55 pages : |b illustrations, tables ; |c 27 cm. | ||
336 | |a text |b txt |2 rdacontent. | ||
337 | |a unmediated |b n |2 rdamedia. | ||
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490 | 1 | |a Technical memorandum ; |v no. 1262. | |
500 | |a "October 1950." | ||
500 | |a NACA TM Number 1262. | ||
500 | |a Translated from Zeitschrift fur Angewandte Mathematik und Mechanik. Volume 15, Number 6, pp. 313-338, December 1935, by the National Advisory Commitee for Aeronautics. | ||
504 | |a Includes bibliographical references. | ||
520 | 3 | |a With applications to meteorology in view, the method of small oscillations is used to investigate the stability of a plane laminar boundary layer in which the density depends in a special way on the distance from the plate. It is found that for a constant Froude number the flow becomes more stable as the Richardson number increases until, at a critical value of the Richardson number that depends on the Froude number, the flow is stable for all disturbance wave lengths and Reynolds numbers. The calculated results are verified by experiment. | |
650 | 0 | |a Laminar flow. |0 http://id.loc.gov/authorities/subjects/sh85074205. | |
650 | 0 | |a Laminar boundary layer. |0 http://id.loc.gov/authorities/subjects/sh2003006140. | |
650 | 0 | |a Turbulence. |0 http://id.loc.gov/authorities/subjects/sh85138753. | |
650 | 0 | |a Boundary layer. |0 http://id.loc.gov/authorities/subjects/sh85016095. | |
650 | 0 | |a Meteorology. |0 http://id.loc.gov/authorities/subjects/sh85084334. | |
650 | 0 | |a Mathematics. |0 http://id.loc.gov/authorities/subjects/sh85082139. | |
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650 | 7 | |a Laminar boundary layer. |2 fast |0 (OCoLC)fst00991078. | |
650 | 7 | |a Laminar flow. |2 fast |0 (OCoLC)fst00991079. | |
650 | 7 | |a Mathematics. |2 fast |0 (OCoLC)fst01012163. | |
650 | 7 | |a Meteorology. |2 fast |0 (OCoLC)fst01018441. | |
650 | 7 | |a Turbulence. |2 fast |0 (OCoLC)fst01159210. | |
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830 | 0 | |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ; |v no. 1262. |0 http://id.loc.gov/authorities/names/no2009014150. | |
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