Theory of radiation from low velocity heated air

D. A. Levin; R. T. Loda; G. V. Candler; C. Park

Theory of radiation from low velocity heated air

D. A. Levin, R. T. Loda, G. V. Candler, C. Park

Aerospace Engineering and Mechanics

Research output: Contribution to conference › Paper › peer-review

Abstract

Application of hypersonic computational fluid dynamics models to low velocity vehicles is examined. The important aspects of the models that were discovered as well as the limits of their applicability are discussed. Modelling aspects such as chemical kinetics, electronic excitation/de-excitation mechanisms, and existence of equilibrium versus non-equilibrium conditions in the flow were examined. Flowfield properties and in-band radiances in the wavelength region of.25μ. in the vicinity of the stagnation streamline are given for a three inch hemisphere. Comparison with recent shock tube data is also shown.

Original language	English (US)
State	Published - Jan 1 1990
Event	28th Aerospace Sciences Meeting, 1990 - Reno, United States Duration: Jan 8 1990 → Jan 11 1990

Other

Other	28th Aerospace Sciences Meeting, 1990
Country/Territory	United States
City	Reno
Period	1/8/90 → 1/11/90

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title = "Theory of radiation from low velocity heated air",

abstract = "Application of hypersonic computational fluid dynamics models to low velocity vehicles is examined. The important aspects of the models that were discovered as well as the limits of their applicability are discussed. Modelling aspects such as chemical kinetics, electronic excitation/de-excitation mechanisms, and existence of equilibrium versus non-equilibrium conditions in the flow were examined. Flowfield properties and in-band radiances in the wavelength region of.25μ. in the vicinity of the stagnation streamline are given for a three inch hemisphere. Comparison with recent shock tube data is also shown.",

author = "Levin, {D. A.} and Loda, {R. T.} and Candler, {G. V.} and C. Park",

year = "1990",

month = jan,

day = "1",

language = "English (US)",

note = "28th Aerospace Sciences Meeting, 1990 ; Conference date: 08-01-1990 Through 11-01-1990",

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TY - CONF

T1 - Theory of radiation from low velocity heated air

AU - Levin, D. A.

AU - Loda, R. T.

AU - Candler, G. V.

AU - Park, C.

PY - 1990/1/1

Y1 - 1990/1/1

N2 - Application of hypersonic computational fluid dynamics models to low velocity vehicles is examined. The important aspects of the models that were discovered as well as the limits of their applicability are discussed. Modelling aspects such as chemical kinetics, electronic excitation/de-excitation mechanisms, and existence of equilibrium versus non-equilibrium conditions in the flow were examined. Flowfield properties and in-band radiances in the wavelength region of.25μ. in the vicinity of the stagnation streamline are given for a three inch hemisphere. Comparison with recent shock tube data is also shown.

AB - Application of hypersonic computational fluid dynamics models to low velocity vehicles is examined. The important aspects of the models that were discovered as well as the limits of their applicability are discussed. Modelling aspects such as chemical kinetics, electronic excitation/de-excitation mechanisms, and existence of equilibrium versus non-equilibrium conditions in the flow were examined. Flowfield properties and in-band radiances in the wavelength region of.25μ. in the vicinity of the stagnation streamline are given for a three inch hemisphere. Comparison with recent shock tube data is also shown.

UR - http://www.scopus.com/inward/record.url?scp=85003758650&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=85003758650&partnerID=8YFLogxK

M3 - Paper

AN - SCOPUS:85003758650

T2 - 28th Aerospace Sciences Meeting, 1990

Y2 - 8 January 1990 through 11 January 1990

ER -

Theory of radiation from low velocity heated air

Abstract

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