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035   $a(PQKBTitleCode)TC0001118517
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100   $a20150119d2013||||  u||         |
101 0 $aeng
135   $aur|n|---|||||
181   $ctxt
182   $cc
183   $acr
200 10$aPrinciples of aeroelasticity
205   $a1st ed.
210   $aNewburyport $cDover Publications$d2013
215   $a1 online resource (948 p.)
225 1 $aDover books on engineering
300   $aDescription based upon print version of record.
311 08$a0-486-61349-6 
327   $aCover; 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
330   $aPrinciple of Aeroelasticity constitutes an attempt to bring order to a group of problems which have coalesced into a distinct and mature subdivision of flight-vehicle engineering. The authors have formulated a unifying philosophy of the field based on the equations of forced motion of the elastic flight vehicle. A distinction is made between static and dynamic phenomena, and beyond this the primary classification is by the number of independent space variables required to define the physical system. Following an introductory chapter on the field of aeroelasticity and its literature, the book
410  0$aDover books on engineering
606   $aAeroelasticity
615  0$aAeroelasticity.
676   $a629.132/362
700   $aBisplinghoff$b Raymond L$0237
701   $aAshley$b Holt$0238
801  0$bAU-PeEL
801  1$bAU-PeEL
801  2$bAU-PeEL
906   $aBOOK
912   $a9911006701403321
996   $aPrinciples of aeroelasticity$9809747
997   $aUNINA