Design and Fabrication of Variable Nozzle for Precooled Turbojet Engine
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA)
2. Waseda University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-7312
Reference7 articles.
1. Taguchi,H.:FiringTestofaHypersonicTurbojetEngineInstalledonaFlightTestVehicle,AIAA-2009-7311.
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