Near equilibrium dissociating boundary layer flows by the method of matched asymptotic expansions / prepared by G.R. Inger.
The approach to equilibrium in a nonequilibrium-dissociating boundary layer flow along catalytic or noncatalytic surfaces is treated from the stand-point of a singular perturbation problem and by use of the method of matched asymptotic expansions. Based on a linearized reaction rate model for a diat...
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| Main Author: | |
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
El Segundo, Calif. :
Aerospace Corporation, Laboratory Operations,
1966.
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| Subjects: |
MARC
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| 027 | |a TR-669(6240-20)-5 | ||
| 035 | |a (OCoLC)ocn1037149948 | ||
| 035 | |a (OCoLC)1037149948 | ||
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| 100 | 1 | |a Inger, George R., |e author. | |
| 245 | 1 | 0 | |a Near equilibrium dissociating boundary layer flows by the method of matched asymptotic expansions / |c prepared by G.R. Inger. |
| 264 | 1 | |a El Segundo, Calif. : |b Aerospace Corporation, Laboratory Operations, |c 1966. | |
| 300 | |a 28 pages ; |c 28 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
| 338 | |a volume |b nc |2 rdacarrier. | ||
| 500 | |a "Air Force report number SSD-TR-66-52." | ||
| 500 | |a "Aerospace report number TR-669(6240-20)-5." | ||
| 500 | |a "March 1966." | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | |a The approach to equilibrium in a nonequilibrium-dissociating boundary layer flow along catalytic or noncatalytic surfaces is treated from the stand-point of a singular perturbation problem and by use of the method of matched asymptotic expansions. Based on a linearized reaction rate model for a diatomic gas which facilitates closed form analysis, a uniformly valid solution for the near-equilibrium behavior is obtained as the composite of appropriate outer and inner solutions. It is shown that under near-equilibrium conditions, the primary nonequilibrium effects are buried in a thin sublayer near the body surface that is described by the inner solution. Applications of the theory are made to the prediction of heat transfer and atom concentrations for blunt body stagnation point and high speed flat plate flows; the results agree with the near-equilibrium behavior predicted by numerical solutions. (Author) | ||
| 650 | 0 | |a Boundary layer. |0 http://id.loc.gov/authorities/subjects/sh85016095. | |
| 650 | 0 | |a Asymptotic expansions. |0 http://id.loc.gov/authorities/subjects/sh85009056. | |
| 650 | 1 | 7 | |a Boundary layer) |2 dtict. |
| 650 | 1 | 7 | |a (Rarefied gas dynamics. |2 dtict. |
| 650 | 2 | 7 | |a Frozen equilibrium flow. |2 dtict. |
| 650 | 2 | 7 | |a Gas flow. |2 dtict. |
| 650 | 2 | 7 | |a Supersonic flow. |2 dtict. |
| 650 | 2 | 7 | |a Perturbation theory. |2 dtict. |
| 650 | 2 | 7 | |a Equilibrium(physiology) |2 dtict. |
| 650 | 2 | 7 | |a Dissociation. |2 dtict. |
| 650 | 2 | 7 | |a Stagnation point. |2 dtict. |
| 650 | 2 | 7 | |a Hypersonic characteristics. |2 dtict. |
| 650 | 2 | 7 | |a Blunt bodies. |2 dtict. |
| 650 | 2 | 7 | |a Walls. |2 dtict. |
| 650 | 2 | 7 | |a Flat plate models. |2 dtict. |
| 650 | 2 | 7 | |a Asymptotic series. |2 dtict. |
| 650 | 1 | 7 | |a Fluid mechanics. |2 scgdst. |
| 710 | 2 | |a Aerospace Corporation. |b Laboratory Operations. |0 http://id.loc.gov/authorities/names/n79121241. | |
| 907 | |a .b101337759 |b 03-19-20 |c 05-23-18 | ||
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| 907 | |a .b101337759 |b 07-12-18 |c 05-23-18 | ||
| 944 | |a MARS - RDA ENRICHED | ||
| 907 | |a .b101337759 |b 05-23-18 |c 05-23-18 | ||
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| 952 | f | f | |p Can circulate |a University of Colorado Boulder |b Boulder Campus |c Norlin |d Norlin Library - Government Information - US |e D 301.71:66-52 |h Superintendent of Documents classification |i document |m U183073495834 |n 1 |