发明名称 |
System and method for calculating aerodynamic performance of tilting wing aircraft |
摘要 |
Aerodynamic performance parameters for aircraft configurations are calculated using an aerodynamic performance system and method. The aerodynamic performance system in a workstation includes a processor circuit having a processor and a memory. Additionally, the system includes aerodynamic performance logic stored on the memory and executable by the processor. The aerodynamic performance logic includes logic that calculates a number of aerodynamic performance parameters for a configuration. Further, the logic generates an aerodynamic performance report to be sent to a client via a network. The aerodynamic performance report lists at least one of the aerodynamic performance parameters.
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申请公布号 |
US6553333(B1) |
申请公布日期 |
2003.04.22 |
申请号 |
US20010871232 |
申请日期 |
2001.05.31 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE |
发明人 |
SHENK BARTH W. |
分类号 |
B64F5/00;G06F17/50;(IPC1-7):G05D13/00 |
主分类号 |
B64F5/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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