000 00595pam a2200169a 44500
008 160408b1980 xxu||||| |||| 00| 0 eng d
082 _a629.13434
_bB644t
100 _aBoppe, Charles W.
245 1 _aTRANSONIC FLOW FIELD ANALYSIS FOR WING-FUSELAGE CONFIGURATIONS
260 _aWashington
_bNational Aeronautics And Space And Administration
_c1980
300 _avii,152
440 _aU. S. National Aeronautics And Space Administration Nasa. Cortractor Report
_vCr-3243
650 _aAeroplanes -- Fuselage
650 _aAerodynamics -- Transonic
964 _gCIRC
997 _aA67647 C
999 _c299937
_d299937