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Density and Speed of Sound Measurements of Jet A and S-8 Aviation Turbine Fuels
Published
Author(s)
Stephanie L. Outcalt, Arno R. Laesecke, Malte B. Freund
Abstract
The density and speed of sound were measured for three compositions of aviation jet fuel A, and a synthetic fuel (S-8) derived from the Fischer-Tropsch process. Measurements of density and speed of sound were carried out at ambient pressure (83 kPa) with a rapid characterization instrument from 278.15 K to 343.15 K. Density measurements of the compressed liquids ranged from 270 K to 470 K with pressures to 30 MPa. A total of 529 experimental points are reported. The density measurements are correlated within 0.1 % with a modified Tait equation of state, and adiabatic compressibilities are derived from the density and speed of sound data at ambient pressure.
Outcalt, S.
, Laesecke, A.
and Freund, M.
(2009),
Density and Speed of Sound Measurements of Jet A and S-8 Aviation Turbine Fuels, Energy and Fuels, [online], https://tsapps.nist.gov/publication/get_pdf.cfm?pub_id=832406
(Accessed October 10, 2025)