Accession Number:

AD0610329

Title:

TEMPERATURE OF A CONE IN SUPERSONIC FLOW WITH CONSIDERATION OF RADIATION,

Personal Author(s):

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Report Date:

1965-01-15

Abstract:

It is shown that the solution of laminary boundary equations on a cone with consideration of the radiation effect can be reduced to the solution of equations similar to corresponding equations for a plate. It is demonstrated that the radiation of an absolutely heat conductive cone is sq. rt. 32 from the radiation of an absolutely heat conductive plate, and absolutely nonconductive cone approximately with an accuracy of up to 2 - sq. rt. 33 of the radiation of an absolutely non heat conductive plate. Author

Supplementary Note:

Unedited rough draft trans. of mono. Sbornik Teoreticheskikh Rabot po Aerodinamike, Moscow, 1957, p. 222-229.

Pages:

0012

Descriptors:

File Size:

0.00MB

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