000 00425pam a2200133a 44500
082 _aNACA
_bTN 2264
100 _aChapman,Dean R
245 1 _aAIRFOIL PROFILES FOR MINIMUM PRESSURE DRAG AT SUPERSONIC VELOCITIES - GENERAL ANALYSIS WITH APPLICATION TO LINEARIZED SUPERSONIC FLOW
260 _a
_bNaca, Washington
_c
300 _a38
500 _aBound With Naca Tn 2260-63,2265-70
964 _gCIRC
997 _aTR15642 C
999 _c400590
_d400590