|
|
|
|
| LEADER |
01091nam a2200217 a 4500 |
| 001 |
693611 |
| 005 |
20171111230500.0 |
| 008 |
070605s1978 gr r 000 0 eng d |
| 040 |
|
|
|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
|
|a McClinton, C. R.
|
| 245 |
1 |
0 |
|a Interaction between step fuel injectors on opposite walls in a supersonic combustor model/
|c Charles R. McClinton ; Langley Research Center
|
| 260 |
|
|
|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Office,
|c 1978
|
| 300 |
|
|
|a 60 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 1174
|
| 504 |
|
|
|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Injectors
|
| 650 |
|
0 |
|a Combustion engineering
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Office
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Office
|
| 710 |
2 |
|
|a Langley Research Center
|
| 952 |
|
|
|a GR-KoDPT
|b 59cc1fd46c5ad13446f86add
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
