Matched-filter and stochastic-simulation-based methods of gust loads prediction
- Author
- SCOTT, R. C1 ; POTOTZKY, A. S; PERRY, B. III1
[1] NASA, Langley res. cent., aeroelasticity branch, Hampton VA 23681-0001, United States - Conference name
- American Institut of Aeronautics and Astronautics. Structures, structural dynamics, and materials conference (34 ; La Jolla CA 1993-04-28)
- Source
Journal of aircraft. 1995, Vol 32, Num 5, pp 1047-1055 ; ref : 10 ref
- CODEN
- JAIRAM
- ISSN
- 0021-8669
- Scientific domain
- Aeronautics astronautics; Mechanical engineering; Mechanics acoustics; Transportation
- Publisher
- American Institute of Aeronautics and Astronautics, Reston, VA
- Publication country
- United States
- Document type
- Conference Paper
- Language
- English
- Keyword (fr)
- Avion Aéronef Charge Croisement niveau Méthode analyse Rafale Réponse impulsion Système commande Système non linéaire
- Keyword (en)
- Airplane Aircraft Load Level crossing Analysis method Gust Pulse response Control system Non linear system
- Keyword (es)
- Avión Aeronave Carga Cruce nivel Método análisis Ráfaga Respuesta impulsión Sistema control Sistema no lineal
- Classification
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D15 Ground, air and sea transportation, marine construction / 001D15J Miscellaneous transportation
- Discipline
- Building. Public works. Transport. Civil engineering
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 3691083
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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DOI
10.2514/3.46835 
https://dx.doi.org/10.2514/3.46835
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