Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3712
Reference30 articles.
1. 2Giesing, J.P.; Kalman, T.P.; and Rodden, W.P. "Subsonic Unsteady Aerodynamics for General Configurations, Part I. Direct Application of the Nonplanar Doublet Lattice Method. Report AFFDL-TR-71-5, November 1971.
2. Computation of Unsteady Transonic Flows by the Indicial Method
3. A state-space model of unsteady aerodynamics in a compressible flow for flutter analyses
4. Unsteady Transonic Aerodynamics
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