000 00572 a2200265 4500
001 12088
020 _a0
041 _aeng
080 _a629.136.3:533.6 Bar
245 _aDistributed vortex method for computing the vortex field of a missile
250 _a
260 _aHampton
260 _bNASA Langley Res. Center,
260 _c1978
300 _a16 p.
300 _c28 cm
490 _a
100 _aBarger, Raymond L.
700 _a
650 _a
650 _aVortex-motion
650 _aGuided missiles-Aerodynamics
942 _cBK
942 _2UDC
999 _c14048
_d14048