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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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