000 00430pam a2200133a 44500
082 _aNASA
_bTN D-6656
100 _aAbel,I
245 1 _aA WIND-TUNNEL EVALUATION OF ANALYTICAL TECHNIQUES FOR PREDICTING STATIC STABILITY AND CONTROL CHARACTERISTICS OF FLEXIBLE AIRCRAFT
260 _a
_bNasa, Washington, D.C.
_c1972
300 _a68
500 _aBound With Nasa Tn D-6650-55, 6657-59.
964 _gCIRC
997 _aTR12290 C
999 _c396928
_d396928