02505nam 22005533 450 991100670140332120230803040402.01-5231-2502-00-486-78316-2(CKB)3710000000334917(EBL)1919842(SSID)ssj0001118517(PQKBManifestationID)12473138(PQKBTitleCode)TC0001118517(PQKBWorkID)11106943(PQKB)10385804(MiAaPQ)EBC1919842(Au-PeEL)EBL1919842(CaONFJC)MIL563612(OCoLC)868279855(EXLCZ)99371000000033491720150119d2013|||| u|| |engur|n|---|||||txtccrPrinciples of aeroelasticity1st ed.Newburyport Dover Publications20131 online resource (948 p.)Dover books on engineeringDescription based upon print version of record.0-486-61349-6 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; IndexPrinciple 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 bookDover books on engineeringAeroelasticityAeroelasticity.629.132/362Bisplinghoff Raymond L237Ashley Holt238AU-PeELAU-PeELAU-PeELBOOK9911006701403321Principles of aeroelasticity809747UNINA