Aircraft Structures for Engineering Students 4E Megson , T.H.G (구조역학 4…
페이지 정보
작성일 19-09-15 15:21본문
Download : Aircraft Structure 4판 megson 솔루션구조역학 4판.pdf
설명
Aircraft Structures for Engineering Students 4판 solution(구조역학)
순서
Aircraft Structures
for engineering students
Fourth Edition
Solutions Manual
T. H. G. Megson
This page intentionally left blank
Solutions Manual
Solutions to Chapter 1 Problems
S.1.1
The principal stresses are given directly by Eqs (1.11) and (1.12) in which σx = 80 N/mm2 , σy = 0 (or vice versa) and τxy = 45 N/mm2 . Thus, from Eq. (1.11) σI = i.e. σI = 100.2 N/mm2 From Eq. (1.12) σII = i.e. σII = ?20.2 N/mm2 The directions of the principal stresses are de?ned by the angle θ in Fig. 1.8(b) in which θ is given by Eq. (1.10). Hence tan 2θ = which gives θ = 24? 11 and θ = 114? 11 2 × 45 = 1.125 80 ? 0 80 1 ? 802 + 4 × 452 2 2 80 1 802 + 4 × 452 + 2 2
It is cle…(省略)
2007. 2. 25
Aircraft Structures for Engineering Students 4E Megson , T.H.G (구조역학 4판 solution )
Download : Aircraft Structure 4판 megson 솔루션구조역학 4판.pdf( 60 )
구조역학,Aircraft,Structures,Engineering,Students,4판,솔루션,기계설계,솔루션
Aircraft Structures for Engineering Students 4판 솔루션(구조역학)Megson T.H.G 저2007. 2. 25 , Aircraft Structures for Engineering Students 4E Megson , T.H.G (구조역학 4판 솔루션 )기계설계솔루션 , 구조역학 Aircraft Structures Engineering Students 4판 솔루션
솔루션/기계설계
Megson T.H.G 저
다.