New experimental data are presented for the vapor−liquid equilibria in the binary systems nitrogen + methane, nitrogen + ethane, and methane + ethane including data for the saturated liquid densities covering a temperature range of 130 K to 270 K and pressures up to 10.1 MPa. On the basis of the new experimental data for these binary mixtures, which may be regarded as model mixtures, the performance of the widely used group contribution equations of state VTPR and PSRK was investigated. These studies focused on the equations' ability to represent accurately saturated liquid densities over a wide range of temperatures and pressures when a constant volume translation was applied.

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Germany's Fifth Aeronautical Research Program (LuFo-V) gives the framework for the thermoelectric energy recuperation for aviation (TERA) project, which focuses on the positioning of thermoelectricity by means of a holistic reflection of technological possibilities and challenges for the adoption of thermoelectric generators (TEG) to aircraft systems. The aim of this paper is to show the project overview and some first estimations of the performance of an integrated TEG between the hot section of an engine and the cooler bypass flow. Therefore, casing integration positions close to different components are considered such as high-pressure turbine (HPT), low-pressure turbine (LPT), nozzle, or one of the interducts, where the temperature gradients are high enough for efficient TEG function. TEG efficiency is then to be optimized by taking into account occurring thermal resistance, heat transfer mechanisms, efficiency factors, as well as installation and operational system constrains like weight and space.

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