Estimation of flutter boundary from random responses due to turbulence at subcritical speeds
- 1 October 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (10), 862-868
- https://doi.org/10.2514/3.44737
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Dynamic Stability Measurements from Tunnel Unsteadiness Excited Random ResponseJournal of Aircraft, 1980
- Wind-Tunnel Technique for Determining Stability Derivatives from Cable-Mounted ModelsJournal of Aircraft, 1978
- Survey of European Ground and Flight Vibration Test MethodsSAE International Journal of Advances and Current Practices in Mobility, 1976
- Canonical Correlation Analysis of Time Series and the Use of an Information CriterionPublished by Elsevier BV ,1976
- The random decrement technique applied to the YF-16 flight flutter testsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Maximum Likelihood Identification of Aircraft Stability and Control DerivativesJournal of Aircraft, 1974
- Estimation of power spectra with finite-order autoregressive modelsIEEE Transactions on Automatic Control, 1973
- Statistical predictor identificationAnnals of the Institute of Statistical Mathematics, 1970
- Prediction of flutter onset speed based on flight testing at subcritical speedsJournal of Aircraft, 1964
- Elementary MatricesPublished by Cambridge University Press (CUP) ,1938