000 00720nam a2200193 4500
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040 _cIIT Kanpur
041 _aeng
100 _aNelms, P. Walter
245 _aEffect of wing elevation incidence and camber on the aerodynamic characteristics of arepresentative hypersonic cruise configuration at mach numbers from 0.65 to 10.70. [NASA TN D-6049]
_cWalter P. Nelms and John A. Axelson
260 _aWashington, D. C.
_bNASA
_c1970
300 _a73p
440 _aNational Aeronautics and Space Administration (NASA)
505 _atechnical report NASA
650 _a aerodynamic
700 _aAxelson, A. John
942 _cTR
999 _c563387
_d563387