33th Congress of the International Council of the Aeronautical Sciences

07 - Systems, Subsystems and Equipment

MATHEMATICAL MODELLING AND ANALYSIS OF THERMAL MANAGEMENT SYSTEM ARCHITECTURE FOR HYPERSONIC AIRCRAFT

S. Nambiar¹, D. Ferreto¹; ¹Politecnico di Torino, Italy

Recent high speed aircraft design studies, like STRATOFLY MR3, were done to increase the TRL of aircraft and optimizing its performance within the supersonic range. Also these studies indicated the importance of aircraft systems interface analysis, in increasing the TRL of the aircraft. This paper presents a mathematical model for the TEMS taking STRATOFLY MR3 aircraft as the baseline, based on Conceptual Multi-Disciplinary Optimization (CMDO).


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