LEADER 03252nam  22006733u 450 
001 9911006520803321
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010   $a9780486267302
010   $a048626730X
010   $a9781621986157
010   $a1621986152
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035   $a(EBL)1893139
035   $a(SSID)ssj0000890055
035   $a(PQKBManifestationID)12353035
035   $a(PQKBTitleCode)TC0000890055
035   $a(PQKBWorkID)10883181
035   $a(PQKB)10445906
035   $a(MiAaPQ)EBC1893139
035   $a(Au-PeEL)EBL1893139
035   $a(OCoLC)898421265
035   $a(Perlego)112875
035   $a(EXLCZ)993460000000121610
100   $a20141222d2013||||  u||         |
101 0 $aeng
135   $aur|n|---|||||
181   $ctxt
182   $cc
183   $acr
200 10$aAircraft Structures
205   $a1st ed.
210   $aNewburyport $cDover Publications$d2013
215   $a1 online resource (1155 p.)
225 1 $aDover Books on Aeronautical Engineering
300   $aDescription based upon print version of record.
311 08$a9780486485805 
311 08$a0486485803 
327   $aCover Page; Title Page; Copyright Page; PREFACE; CONTENTS; 1. EQUILIBRIUM OF FORCES; 2. SPACE STRUCTURES; 3. INERTIA FORCES AND LOAD FACTORS; 4. MOMENTS OF INERTIA, MOHR'S CIRCLE; 5. SHEAR AND BENDING-MOMENT DIAGRAMS; 6. SHEAR AND BENDING STRESSES IN SYMMETRICAL BEAMS; 7. BEAMS WITH UNSYMMETRICAL CROSS SECTIONS; 8. ANALYSIS OF TYPICAL MEMBERS OF SEMIMONOCOQUE STRUCTURES; 9. SPANWISE AIR-LOAD DISTRIBUTION; 10. EXTERNAL LOADS ON THE AIRPLANE; 11. MECHANICAL PROPERTIES OF AIRCRAFT MATERIALS; 12. JOINTS AND FITTINGS; 13. DESIGN OF MEMBERS IN TENSION, BENDING, OR TORSION
327   $a14. DESIGN OF COMPRESSION MEMBERS15. DESIGN OF WEBS IN SHEAR; 16. DEFLECTIONS OF STRUCTURES; 17. STATICALLY INDETERMINATE STRUCTURES; 18. SPECIAL METHODS OF ANALYSIS; APPENDIX; INDEX; Back Cover
330   $aStill relevant decades after its 1950 publication, this legendary reference text on aircraft stress analysis is considered the best book on the subject. It emphasizes basic structural theory, which remains unchanged with the development of new materials and construction methods, and the application of the elementary principles of mechanics to the analysis of aircraft structures. Suitable for undergraduate students, this volume covers equilibrium of forces, space structures, inertia forces and load factors, shear and bending stresses, and beams with unsymmetrical cross sections. Additional topi
410  0$aDover Books on Aeronautical Engineering
606   $aAirframes
606   $aMechanical Engineering$2HILCC
606   $aEngineering & Applied Sciences$2HILCC
606   $aAeronautics Engineering & Astronautics$2HILCC
615  0$aAirframes.
615  7$aMechanical Engineering
615  7$aEngineering & Applied Sciences
615  7$aAeronautics Engineering & Astronautics
676   $a629.134/31
686   $aSCI084000$2bisacsh
700   $aPeery$b David J$03695
801  0$bAU-PeEL
801  1$bAU-PeEL
801  2$bAU-PeEL
906   $aBOOK
912   $a9911006520803321
996   $aAircraft structures$9112005
997   $aUNINA