LEADER 03361nam 22006613u 450 001 9911007077403321 005 20230803022940.0 010 $a0-486-13243-9 010 $a1-62198-657-8 035 $a(CKB)2550000001186473 035 $a(EBL)1894873 035 $a(SSID)ssj0000956078 035 $a(PQKBManifestationID)12459311 035 $a(PQKBTitleCode)TC0000956078 035 $a(PQKBWorkID)10957497 035 $a(PQKB)11156996 035 $a(MiAaPQ)EBC1894873 035 $a(Au-PeEL)EBL1894873 035 $a(CaONFJC)MIL565844 035 $a(OCoLC)868271148 035 $a(EXLCZ)992550000001186473 100 $a20141222d2013|||| u|| | 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aAeroelasticity 205 $a1st ed. 210 $aNewburyport $cDover Publications$d2013 215 $a1 online resource (1577 p.) 225 1 $aDover Books on Aeronautical Engineering 300 $aDescription based upon print version of record. 311 08$a0-486-69189-6 311 08$a1-306-34593-6 327 $aCover; Halftitle Page; Title Page; Copyright Page; Preface Page; Contents; Chapter 1. Introduction to Aeroelasticity; Chapter 2. Deformations of Airplane Structures Under Static Loads; Chapter 3. Deformations of Airplane Structures Under Dynamic Loads; Chapter 4. Approximate Methods of Computing Natural Mode Shapes and Frequencies; Chapter 5. Aerodynamic Tools: Two- and Three-Dimensional in Compressible Flow; Chapter 6. Aerodynamic Tools: Compressible Flow; Chapter 7. Wings and Bodies in Three-Dimensional Unsteady Flow; Chapter 8. Static Aeroelastic Phenomena; Chapter 9. Flutter 327 $aChapter 10. Dynamic Response PhenomenaChapter 11. Aeroelastic Model Theory; Chapter 12. Model Design and Construction; Chapter 13. Testing Techniques; Appendices. Mathematical Tools; A Matrices; B Integration by weighting numbers; C Linear systems; References; Author Index; Subject Index 330 $a Designed as both a textbook for advanced engineering students and a reference book for practicing engineers, this highly regarded work deals not only with the practical aspects of aeroelasticity, but the aerodynamic and structural tools upon which these rest. Accordingly, the book divides roughly into two halves: the first deals with the tools and the second with applications of the tools to aeroelastic phenomena.Topics include deformation of airplane structures under static and dynamic loads, approximate methods of computing natural mode shapes and frequencies, two-and three-dimensional inco 410 0$aDover Books on Aeronautical Engineering 606 $aAeroelasticity 606 $aMechanical Engineering$2HILCC 606 $aEngineering & Applied Sciences$2HILCC 606 $aAeronautics Engineering & Astronautics$2HILCC 615 0$aAeroelasticity. 615 7$aMechanical Engineering 615 7$aEngineering & Applied Sciences 615 7$aAeronautics Engineering & Astronautics 676 $a629.132/362 700 $aBisplinghoff$b Raymond L$0237 701 $aAshley$b Holt$0238 701 $aHalfman$b Robert L$0239 801 0$bAU-PeEL 801 1$bAU-PeEL 801 2$bAU-PeEL 906 $aBOOK 912 $a9911007077403321 996 $aAeroelasticity$91411495 997 $aUNINA