|
|
|
|
LEADER |
00000cam#a22000003a#4500 |
001 |
INGC-MON-09779 |
003 |
AR-LpUFI |
005 |
20221019003854.0 |
008 |
060510s1989 |||a fr||||| |0 0|eng d |
020 |
|
|
|a 1884885500
|
080 |
|
|
|a 629.7.01
|
100 |
1 |
|
|a Roskam, Jan.
|9 282986
|
245 |
0 |
0 |
|a Airplane design. Part V :
|b Component weight estimation.
|
250 |
|
|
|a 2nd. print., 3th. print. .
|
260 |
|
|
|a Kansas :
|b DARcorporation,
|c 1989, 2003.
|
300 |
|
|
|a 209 p. + errata 8 p. :
|b il. ;
|c 28 cm..
|
440 |
0 |
0 |
|a Airplane Design: Part V
|9 284148
|
520 |
|
|
|a Introduction. 2- Class I method for estimating airplane component weights. 3- Class I method for estimating airplane inertias. 4- Class II method for estimating airplane component weights. 5- Class II Method for estimating structure weight. 6- Class II method for estimating powerplant weight. 7- Class II method for estimating fixed equipment weight. 8- Locating component centers of gravity. 9- Class II weight and balance analysis. 10- Clas II method for estimating airplane inertias.
|
599 |
|
|
|a Tomo:V Ubic.:629.7.01 ROS Ej.1 PRES
|
650 |
1 |
4 |
|a DISEÑO DE AERONAVES
|9 272447
|
650 |
1 |
4 |
|a ESTIMACION DEL PESO
|9 284149
|
650 |
1 |
4 |
|a PESO ESTRUCTURAL
|9 284150
|
650 |
1 |
4 |
|a MOMENTO DE INERCIA
|9 283134
|
650 |
1 |
4 |
|a FACTOR DE CARGA
|9 284151
|
650 |
1 |
4 |
|a ANALISIS DE PESOS
|9 284152
|
929 |
|
|
|a 37998 DON Canal
|
942 |
|
|
|c LIB
|6 _
|
959 |
|
|
|a MON
|
960 |
|
|
|a 10463
|
970 |
|
|
|a Registro convertido en forma automatizada
|
990 |
|
|
|a GBY
|
999 |
|
|
|a LC
|c 9777
|d 9777
|
040 |
|
|
|a AR-LpUFI
|c AR-LpUFI
|