000 00614 a2200169 4500
001 62597
082 _a629.134353 ADN / PR 1425
090 _c37202
_d37202
100 _aAdnan Latif Mughal
245 _aDesign and integration of aerodynamic compensating pitot static tube for a supersonic aircraft
260 _aRisalpur
_bAerospace Engg Dept, CAE NUST, Risalpur
_c2004
300 _axv, 96p.
500 _aMS thesis
600 _xpitot static tube for a supersonic aircraft
650 _apitot static tube for a supersonic aircraft
655 _apitot static tube for a supersonic aircraft
942 _aNUST-CAE
_k629.134353 ADN / PR 1425
999 _c297670
_d297670