NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
System Identification and Uncertainty Quantification Using Orthogonal Excitations and the Semi-span Super Sonic Transport (S4T) ModelOrthogonal harmonic multisine excitations were utilized in a wind tunnel test and in simulation of the SemiSpan Supersonic Transport model to assess aeroservoelastic characteristics. Fundamental issues associated with analyzing sinusoidal signals were examined, including spectral leakage, excitation truncation, and uncertainties on frequency response functions and mean-square coherence. Simulation allowed for evaluation of these issues relative to a truth model, while wind tunnel data introduced real-world implementation issues.
Document ID
20120008371
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Heeg, Jennifer
(NASA Langley Research Center Hampton, VA, United States)
Wieseman, Carol D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
April 23, 2012
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 2012-1404
NF1676L-13303
Report Number: AIAA Paper 2012-1404
Report Number: NF1676L-13303
Meeting Information
Meeting: 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Honolulu, HI
Country: United States
Start Date: April 23, 2012
End Date: April 26, 2012
Sponsors: American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, American Society for Composites, American Society of Civil Engineers, American Helicopter Society, Inc.
Funding Number(s)
WBS: WBS 984754.02.07.07.20.06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available