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00926nam a2200241 a 4500 |
| 001 |
787911 |
| 005 |
20171111231157.0 |
| 008 |
080602s1975 gr r 000 0 eng d |
| 040 |
|
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|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
|
|a Weilmuenster, K. James
|
| 245 |
1 |
0 |
|a A finite-difference analysis of the nozzle starting process in an expansion tunnel/
|c K. James Weilmuenster
|
| 260 |
|
|
|a Washington:
|b NASA,
|c 1975
|
| 300 |
|
|
|a 47 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
|
|a NASA technical note
|v 8105
|
| 504 |
|
|
|a Βιβλιογραφία: σ. 25-26
|
| 650 |
|
0 |
|a Shock tubes
|
| 650 |
|
0 |
|a Unsteady flow (Aerodynamics)
|
| 650 |
|
0 |
|a Jet nozzles
|
| 650 |
|
0 |
|a Finite differences
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|
| 710 |
2 |
|
|a Langley Research Center
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration
|
| 952 |
|
|
|a GR-KoDPT
|b 59cc2db96c5ad13446fa8474
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
