000 00716nam a22001937a 4500
003 OSt
005 20220620101514.0
008 220620b xxu||||| |||| 00| 0 eng d
040 _cIIT Kanpur
041 _aeng
100 _aLampkin, Bedford A.
245 _aWind tunnel investigationof the static and dynamicrotary stability derivativesofa fllat top wing body model at mach numbers of 2.5, 3.0 and 3.5 [NASA TM X-361]
_cBedford A. Lampkin and Kenneth C. Endicott
260 _aWashington, D. C.
_bNational Aeronautics and Space Administration
_c1960
300 _a41p
440 _aNational Aeronautics and Space Administration
650 _aWind -- Tunnel
700 _a Endicott, Kenneth C.
942 _cREF
999 _c565673
_d565673