000
00264pam a2200097a 44500
082
_a
CIT
_b
CIT-15
100
_a
C. L. Kirk
245
1
_a
Analysis of taxying induced vibrations in aircraft by the power spectral density method
260
_a
_b
_c
997
_a
TR3995 C
999
_c
405042
_d
405042