000			00848nam a22001697a 4500
003			OSt
005			20210304165806.0
008			210304b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
082			_aNASA _bTM-75237
100			_aGuiot, R.
245			_aComparison of aerodynamic coefficients obtained from theoretical calculations wind tunnel tests and flight tests data reduction for the alpha jet aircraft _bThe methods by which aerodynamic coefficients are determined and discussed. These include: calculations, wind tunnel experiments and experiments in flight for various prototypes of the Alpha Jet. A comparison of obtained results shows good correlation between expectations and in-flight test results. _cR. Guiot and H. Wunnenberg
650			_aNASA Technical Report
700			_aWunnenberg, H.
942			_cBK
999			_c564262 _d564262