NASA NTRS · 19960012499
Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data
Abstract
The method described in this report is intended to present an overview of a process developed to extract the forebody aerodynamic increments from flight tests. The process to determine the aerodynamic increments (rolling pitching, and yawing moments, Cl, Cm, Cn, respectively) for the forebody strake controllers added to the F/A - 18 High Alpha Research Vehicle (HARV) aircraft was developed to validate the forebody strake aerodynamic model used in simulation.
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Messina, Michael D.. 1995-12-01. Using the HARV simulation aerodynamic model to determine forebody strake aerodynamic coefficients from flight data. https://ntrs.nasa.gov/citations/19960012499
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