000 00569pam a2200169a 44500
005 20200717142924.0
008 181205b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aEhlers, F. Edward
245 1 _aA finite difference method for the solution of the transonic flow around harmonically oscillating wing[NASA CR-2257][Bound contains [NASA CR-2254-60]
260 _c1974
_aWashingtion,D.C.
_bNASA
300 _a78p
440 _aNational Aeronautics and Space Administration (NASA)
650 _aHarmonically
942 _cREF
999 _c393138
_d393138