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Estimating unsteady aerodynamic forces on a cascade in a three-dimensional turbulence fieldAn analytical method has been developed to estimate tne unsteady aerodynamic forces caused by flow field turbulence on a wind tunnel turning vane cascade system (vane set). This method approximates dynamic lift and drag by linearly perturbing the appropriate steady state force equations, assuming that the dynamic loads are due only to free stream turbulence and that this turbulence is homogeneous, isotropic, and Gaussian. Correlation and unsteady aerodynamic effects are also incorporated into the analytical model. Using these assumptions, equations relating dynamic lift and drag to flow turbulence, mean velocity, and vane set geometry are derived. From these equations, estimates for the power spectra and rms (root mean squared value, delta) loading of both lift and drag can be determined.
Document ID
19860039992
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Norman, T. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Johnson, W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 86-0735
Accession Number
86A24730
Distribution Limits
Public
Copyright
Other

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