| 000 | 00911nam a2200277 a 4500 | ||
|---|---|---|---|
| 001 | vtls000000494 | ||
| 003 | UG-KaMUL | ||
| 005 | 20250608164859.0 | ||
| 008 | 031110s1991 nyua b 001 0 eng d | ||
| 020 | _a8122403727 | ||
| 039 |
_a201410030926 _b952 _c201212191346 _d916 _c200909071027 _d964 _c200410181551 _d901 _y200311101844 _zstaff |
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| 040 | _aUG-KaMUL | ||
| 082 | _a629.132323 | ||
| 092 | _a629.132323 YAH | ||
| 100 | 1 | _aYahya, S. M. | |
| 245 | 1 |
_aFundamentals of compressible flow : _bwith aircraft rocket propulsi on / _cS.M. Yahya. |
|
| 250 | _a2nd ed | ||
| 260 |
_aNew Delhi : _bWiley Eastern, _c1991. |
||
| 300 |
_aviii, 605 p. : _bill. ; _c22 cm. |
||
| 504 | _aIncludes bibliographical references (p. 598-599) and index. | ||
| 650 |
_aAirplanes _xCompressions |
||
| 650 |
_aAirplanes _xRocket engines |
||
| 942 |
_2ddc _cBK |
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| 999 |
_c17192 _d17192 |
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