Librescu, Liviu:
Unsteady Magnetoaerodynamic Forces on an Oscillating Circular Cylindrical Shell of Finite Length. Part III: Dynamic Response Problem
Atti della Accademia Nazionale dei Lincei. Classe di Scienze Fisiche, Matematiche e Naturali. Rendiconti Serie 8 64 (1978), fasc. n.1, p. 82-87, (English)
pdf (391 Kb), djvu (243 Kb). | Zbl 0398.76077
Sunto
Quest'ultima Nota, essendo la continuazione delle prime due [1, 2], contiene la deduzione delle equazioni che governano il problema della risposta dinamica e descrive un metodo analitico per risolverle.
Referenze Bibliografiche
[1]
L. LIBRESCU (
1977) -
Unsteady Magnetoaerodynamic Forces on an Oscillating Circular Cylindrical Shell of Finite Length. Part I: Simple Harmonic Motion, «
Atti Accad. Naz. Lincei, Rend. Sc. fis. mat. e nat.»,
62 (4). |
Zbl 0383.76092[2]
L. LIBRESCU (
1977) -
Unsteady Magnetoaerodynamic Forces on an Oscillating Circular Cylindrical Shell of Finite Length. Part II: Transient Solution, «
Atti Accad. Naz. Lincei, Rend. Sc. fis. mat. e nat.»,
63 (6). |
Zbl 0398.76076[3]
L. LIBRESCU (
1969) -
Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell Type Structures (in Romanian),
Publ. House of the Academy of the S.R. Romania. |
Zbl 0335.73027[4] S. M. BELOCZERKOVSKI et al. (1974) - The Motion of a Body Taking into Account the Non-Stationarity of the Gas Flow (in Russian), «Mechanika Tverd. Tela», 3, 35-43.
[5] S. M. BELOCZERKOVSKI et al. (1977) - The System of Analysing the Aeroelastic Characteristics of a Flight Vehicle by Taking into Account the Non-Stationarity of the Gas Flow (in Russian), «Mechanika Tverd. Tela», 3, 109-117.
[6]
S. VASILACH (
1959) -
Calcul opérationnel algébrique des distribution à support dans $\mathbf{R}_{+}^{N}$, $n \ge 1$, «
Rev. de Matéhmat. Pures et Appliq., Acad. Rep. Pop. Roumaine»,
4 (2), 185-219. |
MR 117547[7]
A. F. LEONTEV (
1976) -
Exponential Series (in Russian), «
Publ. House "Nauka"», Moscow. |
MR 584943[8]
T. P. G. LIVERMAN (
1964) -
Generalized Functions and Direct Operational Methods, vol.
I,
Prentice-Hall, Inc., Englewood Cliffs, N.J. |
MR 166568 |
Zbl 0119.10301[9]
Y. FUJIMORI and
Y. K. LIN (
1973) -
Analysis of Airplane Response to Nonstationary Turbulence Including Wing Bending Flexibility, «
A.I.A.A. Journ.»,
2 (3), 334-339. |
Zbl 0258.73030
Con il contributo del Ministero per i Beni e le Attività Culturali