NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Variable-Domain Displacement Transfer Functions for Converting Surface Strains into Deflections for Structural Deformed Shape PredictionsVariable-Domain Displacement Transfer Functions were formulated for shape predictions of complex wing structures, for which surface strain-sensing stations must be properly distributed to avoid jointed junctures, and must be increased in the high strain gradient region. Each embedded beam (depth-wise cross section of structure along a surface strain-sensing line) was discretized into small variable domains. Thus, the surface strain distribution can be described with a piecewise linear or a piecewise nonlinear function. Through discretization, the embedded beam curvature equation can be piece-wisely integrated to obtain the Variable-Domain Displacement Transfer Functions (for each embedded beam), which are expressed in terms of geometrical parameters of the embedded beam and the surface strains along the strain-sensing line. By inputting the surface strain data into the Displacement Transfer Functions, slopes and deflections along each embedded beam can be calculated for mapping out overall structural deformed shapes. A long tapered cantilever tubular beam was chosen for shape prediction analysis. The input surface strains were analytically generated from finite-element analysis. The shape prediction accuracies of the Variable- Domain Displacement Transfer Functions were then determined in light of the finite-element generated slopes and deflections, and were fofound to be comparable to the accuracies of the constant-domain Displacement Transfer Functions
Document ID
20150005777
Acquisition Source
Armstrong Flight Research Center
Document Type
Technical Publication (TP)
Authors
Ko, William L.
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Fleischer, Van Tran
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
April 16, 2015
Publication Date
March 1, 2015
Subject Category
Structural Mechanics
Report/Patent Number
DFRC-E-DAA-TN18962
NASA/TP-2015-218464
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
displacement transfer functions
displacement theory
deflection equations
No Preview Available