000 00721nam a2200205 4500
003 OSt
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040 _cIIT Kanpur
041 _aeng
100 _aHess, Robert W.
245 _aAn experimental study of the flutter of sails having a a delta planform tested from a macnh number of 0.1 to A mach number of 1.9 [NASA TM X-355]
_cRobert W. Hess
260 _aWashington, D. C
_bNational Aeronautics and Space Administration
_c1961
300 _a39p
440 _aNational Aeronautics and Space Administration
440 _aNASA Technical Note
500 _aBound vol. contains NASA TM X 350-396
650 _aDelta platform
942 _cTR
999 _c565672
_d565672