Contaminant Freeze-Out In Heat Exchangers. Volume III - Contaminant Freeze-Out Test Data
Report Number: ASD TDR 63-508 Volume 3
Author(s): Hinkley, R. B., Burke, J. C., Ruccia, F. E., Berthiaume, R. P., Reid, R. C., Drake, E. M., Dingwell, I. W., Weber, M. E.
Corporate Author(s): Arthur D Little, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1963-07
Pages: 378
Contract: AF 33(657)-8695
DoD Project: 3084
DoD Task: 308404
Identifier: AD0418070
Abstract:
As part of an analytical and experimental study of water and carbon dioxide freeze-out in heat exchangers, a test program was conducted covering a wide range of air stream pressures, temperatures, mass flow and concentration conditions. The test program consisted of 42 tests, grouped by objective, into five test series. This volume presents the detail test data obtained in the test program. The test data includes mass flow rates, heat balances, contaminant concentrations at the heat exchanger inlet and outlet, notes on the deposit appearance, and tabulations of heat exchanger pressures and temperatures as functions of time and position for each test. In addition, brief summaries of the data obtained in each test series are included. The overall objectives of this test work and the analyses of the results are presented in Volume II to the basic report.
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Hinkley, R. B., Burke, J. C., Ruccia, F. E., Berthiaume, R. P., Reid, R. C., Drake, E. M., Dingwell, I. W., Weber, M. E.
Corporate Author(s): Arthur D Little, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Date of Publication: 1963-07
Pages: 378
Contract: AF 33(657)-8695
DoD Project: 3084
DoD Task: 308404
Identifier: AD0418070
Abstract:
As part of an analytical and experimental study of water and carbon dioxide freeze-out in heat exchangers, a test program was conducted covering a wide range of air stream pressures, temperatures, mass flow and concentration conditions. The test program consisted of 42 tests, grouped by objective, into five test series. This volume presents the detail test data obtained in the test program. The test data includes mass flow rates, heat balances, contaminant concentrations at the heat exchanger inlet and outlet, notes on the deposit appearance, and tabulations of heat exchanger pressures and temperatures as functions of time and position for each test. In addition, brief summaries of the data obtained in each test series are included. The overall objectives of this test work and the analyses of the results are presented in Volume II to the basic report.
Provenance: Lockheed Martin Missiles & Fire Control