Magnetic Suspension and Balance System for High-Subsonic Wind Tunnel
Author:
Affiliation:
1. Waseda University, Tokyo 169-8555, Japan
2. Japan Aerospace Exploration Agency, Chofu 182-0012, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057679
Reference19 articles.
1. Summary of sting interference effects for cone, missile, and aircraft configurations as determined by dynamic and static measurements
2. Transonic Sting Interference
3. A review of Magnetic Suspension and Balance Systems
4. Development of Magnetic Suspension and Balance System for Intermittent Supersonic Wind Tunnels
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