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Abstract

The computer code AGATHE is described. It is intended to evaluate axially symmetric, vapour limited heat pipes with variable channel cross-section and compressible vapour flow at Mach numbers up to 1 and at all radial Reynolds numbers. Heat input and output is modelled by liquid coolant loops. The code can also be used to evaluate empirical factors describing turbulence. Results of pressure drop calculations in cylindrical evaporators with laminar flow are presented for a wide range of radial Reynolds numbers and Mach numbers. The choking limit is determined as a function of the radial Reynolds number. The validity of the boundary layer approximation is examined by comparison of different calculation methods and test data. No evidence precluding the use of this approximation could be found neither at high radial Reynolds number nor with back flow conditions.

Additional information

Authors: BUSSE C A JRC ISPRA ESTAB. (ITALY) PRENGER F C LOS ALAMOS NATIONAL LABORATORY, LOS ALAMOS (USA) , JRC ISPRA ESTAB. (ITALY);LOS ALAMOS NATIONAL LABORATORY, LOS ALAMOS (USA)
Bibliographic Reference: 5TH INTERNATIONAL HEAT PIPE CONFERENCE, TSUKUBA SCIENCE CITY (JAPAN), MAY 14-18, 1984 WRITE TO CEC LUXEMBOURG, DG XIII/A2, POB 1907 MENTIONING PAPER E 31446 ORA
Availability: Can be ordered online
Record Number: 1989123012400 / Last updated on: 1987-01-01
Category: PUBLICATION
Available languages: en
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