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Supersonic Transport Fluid Evaluation Program
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English
Abstract
With the imminent development of the United States Mach 3 Supersonic Transport (SST), aircraft hydraulic fluid state-of-the-art must take another step forward to meet system performance requirements combined with high temperature environments.
This paper presents results of pumping tests conducted by Douglas Aircraft Company, Inc., on 18 different chemical types of proposed SST hydraulic fluids comprising 50 different fluid combinations. Pump and fluid performance data are presented for all 50 fluids evaluated. A general discussion of fluid properties versus performance is also provided.
Four specific fluid types are considered the best SST hydraulic fluid contenders. They are: chlorosilicone, mineral oil (super refined), perfluoroalkyl, and polyaryl.
Authors
Citation
Galloway, C., "Supersonic Transport Fluid Evaluation Program," SAE Technical Paper 650328, 1965, https://doi.org/10.4271/650328.Also In
References
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- Szebehely “Relation Between Gas Evolution and Physical Properties of Liquids,” Journal of Applied Physics 22 5 627 1951
- LeRoy W. W. Leslie R. L. “Hydraulic Fluid Properties and System Performance.” Vickers Hydraulics Symposium Detroit, Michigan 1963
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- Hays D. F. “Lubrication Review.” ASLE-ASME International Lubrication Conference Washington, D.C. October 1964