Tait-Kirchhoff method for determining rotary and unsteady force derivatives
- Author
- DE DIVITIIS, Nicola1
[1] La Sapienza University, Dipartimento di Ingegneria Meccanica e Aerospaziale, Via Eudossiana, 18, 00184 Rome, Italy - Source
Aerospace science and technology (Imprimé). 2014, Vol 39, pp 384-394, 11 p ; ref : 22 ref
- ISSN
- 1270-9638
- Scientific domain
- Aeronautics astronautics; Mechanics acoustics
- Publisher
- Elsevier, Issy-les-Moulineaux
- Publication country
- France
- Document type
- Article
- Language
- English
- Author keyword
- Cramer-Rao bounds Identification Tait-Kirchhoff model Unsteady and rotational force derivatives
- Keyword (fr)
- Aérodynamique Aéronef Essai en vol Force aérodynamique Manoeuvrabilité Modélisation Planeur Simulation numérique
- Keyword (en)
- Aerodynamics Aircraft Flight test Aerodynamic force Maneuverability Modeling Glider Numerical simulation
- Keyword (es)
- Aerodinámica Aeronave Prueba en vuelo Fuerza aerodinámica Maniobrabilidad Modelización Planeador Simulación numérica
- Classification
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D15 Ground, air and sea transportation, marine construction / 001D15I Air transportation and traffic
- Discipline
- Building. Public works. Transport. Civil engineering
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 29022564
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
10.1016/j.ast.2014.04.013 
https://dx.doi.org/10.1016/j.ast.2014.04.013
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