V.Yu. Aleksandrov  , N.V. Kukshinov , A.N. Prokhorov , A.V. Rudinskiy

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_40101115

In the project HEXAFLY a large-scale model of a high-speed civil aircraft on hydrogen fuel was proposed [1-2]. The concept of this model formed the basis of the HEXAFLY-INT project [3]. The view of the investigated aircraft is shown in Fig. 1. This project involves the Central Institute of Aviation Motors (CIAM), Moscow, Russia, in the part of preparing, conducting and analyzing the ground tests of the facility module. The geometry of the facility module (Fig. 2) differs from the original one in that the facility module has the intake of a simplified configuration. The facility module has two fuel supply zones, one at the entrance to the inner flow path, the other in the middle of the expanding combustion chamber.

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In Categories: High-Speed Aerodynamics and Aerothermodynamics, HiSST 2018, Hypersonic Aerodynamics, Hypersonic Flight Dynamics, Supersonic and Hypersonic Aircraft Design, Testing and Evaluation, Thermal and Energy Management Systems
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