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| LEADER |
01272Cam#a22004453a#4500 |
| 001 |
INGC-MON-10028 |
| 003 |
AR-LpUFI |
| 005 |
20221019003924.0 |
| 008 |
060510s1999 |||a fr||||| |0 0|eng d |
| 020 |
|
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|a 1563472810
|
| 080 |
|
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|a 629.7.01
|
| 100 |
0 |
|
|a Raymer, Daniel P.
|9 285093
|
| 245 |
0 |
0 |
|a Aircraft Design :
|b A conceptual Approach
|
| 250 |
|
|
|a 3a ed.
|
| 260 |
|
|
|a Reston :
|b AIAA,
|c 1999.
|
| 300 |
|
|
|a 923 p.
|
| 440 |
0 |
0 |
|a AIAA Edu
|9 283009
|
| 599 |
|
|
|a Ubic.:629.7.01 RAY Ej.1 PRES A2180 Ubic.:629.7.01 RAY Ej.2 PRES
|
| 650 |
1 |
4 |
|a PERFILES
|9 281619
|
| 650 |
1 |
4 |
|a PLANTA ALAR
|9 283984
|
| 650 |
1 |
4 |
|a CARGA ALAR
|9 285094
|
| 650 |
1 |
4 |
|a DIMENSIONES
|9 269423
|
| 650 |
1 |
4 |
|a TREN DE ATERRIZAJE
|9 281560
|
| 650 |
1 |
4 |
|a PROPULSION
|9 283619
|
| 650 |
1 |
4 |
|a AERODINAMICA
|9 268671
|
| 650 |
1 |
4 |
|a DISEÑO AERODINAMICO
|9 284494
|
| 650 |
1 |
4 |
|a ESTABILIDAD
|9 264856
|
| 650 |
1 |
4 |
|a CONTROL
|9 263886
|
| 650 |
1 |
4 |
|a PERFORMANCE
|9 281540
|
| 650 |
1 |
4 |
|a MECANICA DE VUELO
|9 271009
|
| 650 |
1 |
4 |
|a ANALISIS DE COSTOS
|9 271159
|
| 650 |
1 |
4 |
|a ATMOSFERA STANDAR
|9 281616
|
| 929 |
|
|
|a 32215 com
|
| 942 |
|
|
|c LIB
|6 _
|
| 959 |
|
|
|a MON
|
| 960 |
|
|
|a 10722
|
| 970 |
|
|
|a Registro convertido en forma automatizada
|
| 990 |
|
|
|a LC
|
| 999 |
|
|
|c 10026
|d 10026
|
| 040 |
|
|
|a AR-LpUFI
|c AR-LpUFI
|