000 00481pam a2200133a 44500
082 _aNASA
_bTN D-7753
100 _aMack,Robert J
245 1 _aEFFECTS OF LEADING-EDGE SWEEP ANGLE AND DESIGN LIFT COEFFICIENT ON PERFORMANCE OF A MDIFIED ARROW WING AT A DESIGN MACH NUMBER OF 2.6
260 _a
_bNasa, Washington, D.C.
_c1974
300 _a49
500 _aBound With Nasa Tn D-7742-51,7754-60 Lack No.7746,7748-7749,7752,7755,7758-7760
964 _gCIRC
997 _aTR15004 C
999 _c399662
_d399662