我が国独自の超音速飛行機やスペースプレーン開発のための飛行実験研究創生事業における空力実験装置複合体の構築 (<特集>2003年度実施の地域との共同研究の報告)

概要

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With the aims of leading and supporting the development studies on supersonic air- and spaceplanes at JAXA,a 21st-century center-of-excellence program project “Research and Development of Technology Basis forNext Generation Space Transportation Systems” and its revision “A Flight Experiment Research ActivityCreation Project” have been proposed. As their precursors, some wind tunnel elements in the proposedAerodynamic Experiment Facility Complex are being constructed. One is a small-scale blowdown/indraftsupersonic wind tunnel with rectangular nozzle flows of Mach 2 and 4 and of 80mm×80mm dimension.Another is a small-scale supersonic Ludwieg tube of Mach 2 and 3. These two wind tunnel elements will beoperated also for hypersonics by addition of an air heater. And the other is the middle-scale supersonic windtunnel with rectangular internal nozzle flows of Mach 2, 3, and 4 and of 400mm×400mm dimension. Theywill be integrated into the Aerodynamic Experiment Facility Complex and used for acquisition ofaerodynamic data for configuration/flight path designs of flight experiment vehicles and supersonicair-/spaceplanes
室蘭工業大学の論文
2004-11-30