000 00506nam a22001577a 4500
005 20201215142738.0
008 201215b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
245 _aHelcopter rotor rotationalnoise predictions based on measured high fequency blade loads [NASA TN D 7624]
_cRobert N. Hoser
260 _aNational Aeronautics and Space Admnistration (NASA)
300 _a82p
505 _aNASA Technical Note 7624
650 _aRotational noise
942 _cREF
999 _c563666
_d563666