Class of nonlinear third-order systems reducible to equivalent linear systems.
Author:
Affiliation:
1. Indian Institute of Science, Bangalore, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4766
Reference15 articles.
1. Scala, M. and Baulknight, C. W. "Transport and Thermodynamic Properties in a Hypersonic Laminar Boundary Layer, Part 1. Properties of the Pure Species/' ARS Journal, Vol.29, 1959, pp.39-45.
2. Dorrance, W. H., Viscous Hypersonic Flow, 1st ed., Mc-Graw-Hill,New York, 1962, Chap. 4, pp.85-91.
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1. Lower bound on forcing amplitude for stability of forced oscillations in a third order non-linear system;Journal of Sound and Vibration;1979-11
2. Application of ultraspherical polynomials to forced oscillations of a third-order non-linear system;Journal of Sound and Vibration;1974-10
3. Equivalent non-linear and linear third-order systems;International Journal of Systems Science;1973-03
4. Equivalent higher order linear and non-linear systems;Journal of Sound and Vibration;1971-06
5. Errata: "A Transformation Theory for the Compressible Turbulent Boundary Layer with Mass Transfer";AIAA Journal;1970-11
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