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20221019003931.0 |
| 008 |
060510s1954 |||a fr||||| |0 0|eng d |
| 080 |
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|a 629.7.02
|
| 100 |
0 |
|
|a Niles, Alfred S.
|9 284410
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| 245 |
0 |
0 |
|a Airplane Structures :
|b Vol.1
|
| 250 |
|
|
|a 4a ed.
|
| 260 |
|
|
|a New York :
|b Wiley,
|c 1954.
|
| 300 |
|
|
|a 607 p.
|
| 599 |
|
|
|a Tomo:1 Ubic.:629.7.02 NIL Ej.2 PRES
|
| 650 |
1 |
4 |
|a ESTRUCTURA DE AERONAVES
|9 284428
|
| 650 |
1 |
4 |
|a TENSIONES
|9 264906
|
| 650 |
1 |
4 |
|a FLEXION
|9 264777
|
| 650 |
1 |
4 |
|a CORTE
|9 265026
|
| 650 |
1 |
4 |
|a TORSION
|9 264832
|
| 650 |
1 |
4 |
|a CALCULO DE ESTRUCTURAS
|9 264475
|
| 650 |
1 |
4 |
|a ANALISIS ESTRUCTURAL
|9 265344
|
| 650 |
1 |
4 |
|a FLEXOTORSION
|9 284418
|
| 650 |
1 |
4 |
|a RETICULADORES
|9 285274
|
| 650 |
1 |
4 |
|a PLACAS
|9 265006
|
| 650 |
1 |
4 |
|a COLUMNAS
|9 265140
|
| 650 |
1 |
4 |
|a VIGAS
|9 264637
|
| 650 |
1 |
4 |
|a BARRAS
|9 265633
|
| 650 |
1 |
4 |
|a TENSIONES COMBINADAS
|9 284155
|
| 650 |
1 |
4 |
|a HIPOTESIS DE ROTURA
|9 285275
|
| 650 |
1 |
4 |
|a VIGA WAGNER
|9 285276
|
| 650 |
1 |
4 |
|a REMACHES
|9 281524
|
| 650 |
1 |
4 |
|a JUNTA REMACHADA
|9 284233
|
| 650 |
1 |
4 |
|a METODO DE LAS FUERZAS
|9 265343
|
| 650 |
1 |
4 |
|a HIPERESTATICOS
|9 285028
|
| 650 |
1 |
4 |
|a PLASTICIDAD
|9 264854
|
| 650 |
1 |
4 |
|a PERFILES
|9 281619
|
| 700 |
0 |
|
|a Newell, Joseph S.
|9 284420
|
| 942 |
|
|
|c LIB
|6 _
|
| 959 |
|
|
|a MON
|
| 960 |
|
|
|a 10784
|
| 970 |
|
|
|a Registro convertido en forma automatizada
|
| 999 |
|
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|c 10086
|d 10086
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| 040 |
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|a AR-LpUFI
|c AR-LpUFI
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