000 02097nam a22001937a 4500
999 _c44789
_d44789
003 OSt
020 _a9780486691893
082 _a629.132362 BIS-A
100 _aBisplinghoft, Raymond
245 _aAeroelasticity
250 _a1st
260 _aNew York
_bDover Publication
_c1955
300 _a860p.
500 _aDesigned 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 incompressible flow, compressible flow, wings and bodies in three-dimensional unsteady flow, static aeroelastic phenomena, flutter, dynamic response phenomena, aeroelastic model theory, model design and construction, testing techniques and more. Chapters have been designed to progress from easy to difficult so that instructors using this book as an elementary text in aeroelasticity will find their purposes served by simply using the first parts of selected chapters. Helpful appendixes deal with such mathematical tools as matrices and linear systems (prerequisites include the usual engineering mathematics courses and advanced calculus}, while many numerical examples are included throughout the text. Engineering students as well as practicing engineers will find this work an unmatched treatment of the topic and an indispensable reference for their libraries.
650 _aAeroelastic Phenomena, Static Aeroelastic Phenomena, Flutter
856 _uhttps://books.google.co.in/books?id=D1Gl4IWHjyUC&printsec=frontcover&dq=Aeroelasticity&hl=en&sa=X&ved=0ahUKEwjyv4OA7dflAhWBN48KHbE5CewQ6AEIKTAA#v=onepage&q=Aeroelasticity&f=false
901 _a29318
942 _2ddc
_cBK