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- W2000283583 abstract "Initial steps in the application o f a low-order panel method computational fluid dynamic (CFD) code to the calculation of aircraft dynamic stability and control (S&C) derivatives are documented. Several capabilities, unique to CFD but not unique to this particular demonstration, are identified and demonstrated in this paper. These unique capabilities complement conventional S&C techniques and they include the ability to: 1) perform maneuvers without the flow-kinematic restrictions and support interference commonly associated with experimental S&C facilities, 2) easily simulate advanced S&C testing techniques, 3) compute exact S&C derivatives with uncertainty propagation bounds, and 4) alter the flow physics associated with a particular testing technique from those observed in a wind or water tunnel test in order to isolate effects. Also presented are discussions about some computational issues associated with the simulation of S&C tests and selected results from numerous surface grid resolution studies performed during the course of the study." @default.
- W2000283583 created "2016-06-24" @default.
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- W2000283583 date "2004-01-05" @default.
- W2000283583 modified "2023-10-16" @default.
- W2000283583 title "Applications of Computational Methods for Dynamic Stability and Control Derivatives" @default.
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- W2000283583 doi "https://doi.org/10.2514/6.2004-377" @default.
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