|
|
|
|
| LEADER |
01165nam a2200229 a 4500 |
| 001 |
703083 |
| 005 |
20171111231043.0 |
| 008 |
081201s1981 gr r 000 0 eng d |
| 040 |
|
|
|a GR-KoDPT
|b gre
|e AACR2
|
| 100 |
1 |
|
|a Kumar, Ajay
|
| 245 |
1 |
0 |
|a Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations/
|c Ajay Kumar
|
| 260 |
|
|
|a Washington:
|b National Aeronautics and Space Administration, Scientific and Technical Information Branch,
|c 1981
|
| 300 |
|
|
|a 27 σ. :
|b εικ. ;
|c 28 εκ.
|
| 490 |
0 |
|
|a NASA technical paper
|v 1940
|
| 504 |
|
|
|a Περιέχει βιβλιογραφικές παραπομπές
|
| 650 |
|
0 |
|a Airplanes
|x Ramjet engines
|x Mathematical models
|
| 650 |
|
0 |
|a Navier-Stokes equations
|x Data processing
|
| 650 |
|
0 |
|a Viscous flow
|x Mathematical models
|
| 710 |
|
|
|a United States
|b National Aeronautics and Space Administration
|b Scientific and Technical Information Branch
|
| 710 |
0 |
|
|a United States.
|b National Aeronautics and Space Administration.
|b Scientific and Technical Information Branch
|
| 710 |
2 |
|
|a Langley Research Center
|
| 952 |
|
|
|a GR-KoDPT
|b 59cc20df6c5ad13446f8935b
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
|
