Principles of aeroelasticity

• Autore: Bisplinghoff Raymond L
• Pubblicazione: Newburyport, : Dover Publications, 2013
• Edizione: 1st ed.
• Descrizione fisica: 1 online resource (948 p.)
• Disciplina: 629.132/362
• Soggetto topico: Aeroelasticity
• Altri autori: AshleyHolt
• Note generali: Description based upon print version of record.
• Nota di contenuto: Cover; Title Page; Copyright Page; Dedication; Contents; 1 - Introduction; 2 - Mathematical Foundations of Aeroelasticity; 3 - Aeroelastic Equations and their Solutions; 4 - Aerodynamic Operators; 5 - Structural Operators; 6 - The Typical Section; 7 - One-Dimensional Structures; 8 - Two-Dimensional Structures; 9 - The Unrestrained Vehicle; 10 - Systems with Time-Varying Coefficients or Nonlinearities; Index
• Sommario/riassunto: Principle of Aeroelasticity constitutes an attempt to bring order to a group of problems which have coalesced into a distinct and mature subdivision of flight-vehicle engineering. The authors have formulated a unifying philosophy of the field based on the equations of forced motion of the elastic flight vehicle. A distinction is made between static and dynamic phenomena, and beyond this the primary classification is by the number of independent space variables required to define the physical system. Following an introductory chapter on the field of aeroelasticity and its literature, the book
• Titolo autorizzato: Principles of aeroelasticity
• ISBN: 1-5231-2502-0; 0-486-78316-2
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9911006701403321
• Lo trovi qui: Univ. Federico II
• Serie: Dover books on engineering