000 00628 a2200241 4500
001 283274
020 _a
041 _aeng
080 _aLNASA TP 2205 : 1984
245 _aInvestigation of installation effects on twin-engine convergent-divergentnozzles
250 _a
260 _aWashington, D.C.
260 _bNational Aeronautics and Space Adminstration
260 _c1983
300 _a189 p.
300 _c
856 _uNASA
490 _aNASA TP 2205 : 1984
700 _a
650 _a
650 _aTwin engine, Convergent-divergent nozzle, Empennage interference, Nozzle drag, Afterbody drag
942 _cPP
942 _2UDC
999 _c243184
_d243184