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Implementation and Testing of Turbulence Models for the F18-HARV SimulationThis report presents three methods of implementing the Dryden power spectral density model for atmospheric turbulence. Included are the equations which define the three methods and computer source code written in Advanced Continuous Simulation Language to implement the equations. Time-history plots and sample statistics of simulated turbulence results from executing the code in a test program are also presented. Power spectral densities were computed for sample sequences of turbulence and are plotted for comparison with the Dryden spectra. The three model implementations were installed in a nonlinear six-degree-of-freedom simulation of the High Alpha Research Vehicle airplane. Aircraft simulation responses to turbulence generated with the three implementations are presented as plots.
Document ID
19980028448
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Yeager, Jessie C.
(Lockheed Martin Corp. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1998
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA/CR-1998-206937
NAS 1.26:206937
Funding Number(s)
CONTRACT_GRANT: NAS1-96014
CONTRACT_GRANT: RTOP 522-35-11-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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