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01522cam#a22005173a#4500 |
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20221019003859.0 |
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060510s1954 |||a fr||||| |0 0|eng d |
| 080 |
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|a 629.7.02
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| 100 |
0 |
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|a Niles, Alfred S.
|9 284410
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| 245 |
0 |
0 |
|a Airplane Structures
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| 250 |
|
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|a 2a ed.
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| 260 |
|
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|a New York :
|b Wiley,
|c 1954.
|
| 300 |
|
|
|a 607 p.
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| 599 |
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|a Tomo:I Ubic.:629.7.02 NIL Ej.1 PRES
|
| 650 |
1 |
4 |
|a ESTRUCTURA DE AERONAVES
|9 284411
|
| 650 |
1 |
4 |
|a REQUERIMIENTO DE DISEÑO
|9 284412
|
| 650 |
1 |
4 |
|a REACCIONES
|9 266073
|
| 650 |
1 |
4 |
|a CORTE
|9 265026
|
| 650 |
1 |
4 |
|a MOMENTO FLECTOR
|9 282632
|
| 650 |
1 |
4 |
|a PROPIEDADES DE MATERIALES
|9 281501
|
| 650 |
1 |
4 |
|a TORSION VIGA SIMPLE
|9 284413
|
| 650 |
1 |
4 |
|a COMPRESION DE COLUMNAS
|9 284414
|
| 650 |
1 |
4 |
|a COMPRESION DE PANELES
|9 284415
|
| 650 |
1 |
4 |
|a ESTRUCTURAS INDETERMINADAS
|9 284416
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| 650 |
1 |
4 |
|a TENSIONES COMBINADAS
|9 284155
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| 650 |
1 |
4 |
|a CARGA CRITICA
|9 284417
|
| 650 |
1 |
4 |
|a CORTE
|9 265026
|
| 650 |
1 |
4 |
|a FLEXION
|9 264777
|
| 650 |
1 |
4 |
|a VIGAS
|9 264637
|
| 650 |
1 |
4 |
|a BARRAS
|9 265633
|
| 650 |
1 |
4 |
|a TORSION
|9 264832
|
| 650 |
1 |
4 |
|a FLEXOTORSION
|9 284418
|
| 650 |
1 |
4 |
|a RETICULADOR
|9 284419
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| 650 |
1 |
4 |
|a DEFORMACION
|9 264991
|
| 650 |
1 |
4 |
|a TENSIONES
|9 264906
|
| 650 |
1 |
4 |
|a REMACHES
|9 281524
|
| 650 |
1 |
4 |
|a JUNTA REMACHADA
|9 284233
|
| 700 |
0 |
|
|a Newell, Joseph S.
|9 284420
|
| 942 |
|
|
|c LIB
|6 _
|
| 959 |
|
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|a MON
|
| 960 |
|
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|a 10515
|
| 970 |
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|a Registro convertido en forma automatizada
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| 999 |
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|c 9826
|d 9826
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| 040 |
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|a AR-LpUFI
|c AR-LpUFI
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