000 00420pam a2200133a 44500
082 _aNACA
_bRM-L55H31
100 _aClements,James B
245 1 _aA THEORETICAL ANALYSIS OF A SIMPLE AERODYNAMIC DEVICE TO IMPROVE THE LONGITUDINAL DAMPING OF A CRUIFORM MISSILE CONFIGURATION AT SUPERSONIC SPEEDS
260 _a
_b
_c1957
300 _a36
500 _aBound With Naca Rm L53a07
964 _gCIRC
997 _aTR3501 C
999 _c402324
_d402324