Feasibility of a Semiconductor Electric Heater for a Hypersonic True Temperature wind Tunnel.
類似資料:
American Institute of Aeronautics and Astronautics |
7
テクニカルペーパー
A Research Program for the Development of a True-Temperature Mach 8-15 Medium-Scale Hypersonic Wind Tunnel
American Institute of Aeronautics and Astronautics |
2
テクニカルペーパー
Transient Start-up Simulations for a Semiconductor Heater for a Mach 7 True Temperature Wind Tunnel
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
High Temperature Storage Heater Technology for Hypersonic Wind Tunnels and Propulsion Test Facilities
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
6
テクニカルペーパー
Electrical Control of a Semiconductor Heater for a Continuous Mach 7 True-Temperature Wind Tunnel
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |