System and method for calculating aerodynamic performance of tilting wing aircraft
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United States of America Patent
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-
Apr 22, 2003
Grant Date -
N/A
app pub date -
May 31, 2001
filing date -
May 31, 2000
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
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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