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Extension of a Kolmogorov Atmospheric Turbulence Model for Time-Based Simulation ImplementationThe development of any super/hypersonic aircraft requires the interaction of a wide variety of technical disciplines to maximize vehicle performance. For flight and engine control system design and development on this class of vehicle, realistic mathematical simulation models of atmospheric turbulence, including winds and the varying thermodynamic properties of the atmosphere, are needed. A model which has been tentatively selected by a government/industry group of flight and engine/inlet controls representatives working on the High Speed Civil Transport is one based on the Kolmogorov spectrum function. This report compares the Dryden and Kolmogorov turbulence forms, and describes enhancements that add functionality to the selected Kolmogorov model. These added features are: an altitude variation of the eddy dissipation rate based on Dryden data, the mapping of the eddy dissipation rate database onto a regular latitude and longitude grid, a method to account for flight at large vehicle attitude angles, and a procedure for transitioning smoothly across turbulence segments.
Document ID
20040105598
Acquisition Source
Langley Research Center
Document Type
Other
Authors
McMinn, John D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1997
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA Paper 97-3532
Report Number: AIAA Paper 97-3532
Distribution Limits
Public
Copyright
Public Use Permitted.
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