000 00287pam a2200097a 44500
082 _aTR
_bACA-70
100 _aE.R.A. Landers
245 1 _aPressure distributions on planar and cruciform delta wing attached to cylindrical bodies in supersonic flow
260 _a
_b
_c
997 _aTR3848 C
999 _c404959
_d404959