000 00462pam a2200133a 44500
082 _aNASA
_bMEMO 1-17-59A -
100 _aDugan,Duane W
245 1 _aESTIMATION OF STATIC LONGITUDINAL STABILITY OF AIRCRAFT CONFIGURATIONS AT HIGH MACH NUMBERS AND AT ANGLES OF ATTACK BETWEEN 0(DEGREE) AND +-180(DEGREE)
260 _a
_bNasa, Washington, D.C.
_c1962
300 _a72
500 _aBound With Nasa Memo 1-8-59a-1-29-59a
964 _gCIRC
997 _aTR7771 C
999 _c393424
_d393424