MIST implements minimum-state method for determining rational approximations of matrix of aerodynamic force coefficients. Accepts complex tabular data representing generalized unsteady aerodynamic forces over set of reduced frequencies. Determines approximations to tabular data in Laplace domain by use of rational functions. Provides capability to select coefficients of denominator in rational approximations, to constrain approximation selectably without increasing size of problem, and determines and emphasizes criticial frequency ranges in determining approximations. Written in ANSI FORTRAN 77.
Program Determines Minimum-State Approximations To Unsteady Aerodynamic Forces
NASA Tech Briefs ; 17 , 7
1993-07-01
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Minimum-State Unsteady Aerodynamic Approximations with Flexible Constraints
Online Contents | 1996
|Minimum-State Unsteady Aerodynamic Approximations with Flexible Constraints
British Library Conference Proceedings | 1995
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