Actuator Disk Implementation in FENSAP- ICE, a 3D Navier- Stokes In- Flight Simulation System

机译：在FENSAPICE（3D Navier-Stokes飞行模拟系统）中执行器磁盘的实现

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来源
《41st Aerospace Sciences Meeting and Exhibit》|2003年|1-7|共7页
会议地点 Reno NV(US)
作者
G. Baruzzi; P. Tran; W. Habashi; J. Narramore;
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作者单位

Newmerical Technologies Int., Montreal, Quebec, Canada;

Newmerical Technologies Int., Montreal, Quebec, Canada;

Newmerical Technologies Int., Montreal, Quebec, Canada;

Bell Helicopter Textron Inc., Fort Worth, TX;

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中图分类航空;
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4. Actuator Disk Implementation in FENSAP- ICE, a 3D Navier- Stokes In- Flight Simulation System [C] . Aerospace Sciences Meeting and Exhibit . 2003

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Actuator Disk Implementation in FENSAP- ICE, a 3D Navier- Stokes In- Flight Simulation System

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